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Hindawi Publishing CorporationAdvances in Acoustics and VibrationVolume 2013 Article ID 903934 6 pageshttpdxdoiorg1011552013903934
Research ArticleAnomalous Dispersion of the 119878
1Lamb Mode
Faiz Ahmad and Takasar Hussain
Centre for Advanced Mathematics and Physics National University of Sciences and Technology H-12 CampusIslamabad 44000 Pakistan
Correspondence should be addressed to Takasar Hussain htakasaryahoocom
Received 30 April 2013 Revised 1 July 2013 Accepted 16 July 2013
Academic Editor Abdelkrim Khelif
Copyright copy 2013 F Ahmad and T Hussain This is an open access article distributed under the Creative Commons AttributionLicense which permits unrestricted use distribution and reproduction in any medium provided the original work is properlycited
The 1198781mode of the Lamb spectrum of an isotropic plate exhibits negative group velocity in a narrow frequency domain This
anomalous behavior is explained analytically by examining the slope of each mode first in its initial state and then near its turningpoints
1 Introduction
The dispersion relation for symmetric Lamb modes propa-gating in an infinite isotropic plate of thickness 2ℎ is given bythe well known Rayleigh-Lamb equation [1]
tan (119901ℎ)tan (119902ℎ)
= minus41199011199021198962
(1199012minus 1198962)2 (1)
where
119901 = radic1205962
1198882
119879
minus 1198962
119902 = radic1205962
1198882
119871
minus 1198962
(2)
In (1) 119888119879and 119888119871 respectively denote the phase speeds of
the transverse and longitudinal bulk waves in the materialAlso120596 and 119896 respectively denote the frequency and thewavenumber of the modeThe phase velocity 119888 of a mode is givenby
119888 =120596
119896 (3)
If 119888 is plotted as a function of the frequency the spectrumappears as in Figure 1 which depicts the spectrum for a steelplate with 119888
119879= 324 kms and 119888
119871= 595 kms
Themost striking feature in Figure 1 is the shape of the 1198781
mode which has a turning point at 119896119879= 2686 and the phase
velocity becomes double valued for 119896119879ℎ in [2686 2873]This
phenomenon of negative group velocity is of great technicalsignificance and has been observed in a large number ofexperiments [2ndash8]
The afore mentioned feature of 1198781mode was first noticed
by Tolstoy and Usdin [9] in 1957 In all isotropic materialswith 120581 = 2 (] = 13) only the 119878
1mode has this ldquoanomalous
behaviorrdquo and other modes behave normally We will call itthe 1198781anomaly An explanation of this peculiar shape ofmode
1198781has posed a challenge since its discovery in 1957For the special case of a material with ] = 13 that is
119888119871= 2119888119879 each of the modes 119878
3119899+1 119899 = 0 1 2 3 exhibits
anomalous behavior [10] Anomalous pairs of modes mayalso occur for certain special values of the Poisson ratio Wewill call it the pair anomaly
Although (1) governs the behavior of all modes anoma-lous or otherwise no simple theory seems to exist whichshould provide a satisfactory explanation of why certainmodes in the spectrum should possess a bulge while othersproceed in a normal manner However certain physicalexplanations of this phenomenon exist In 1983 Whitakerand Haus [11] noted the fact that ldquopropagation of waves withdispersion of this sort has been experimentally verified [2]but the reason for their appearance is not well understoodrdquoThey used the coupled mode theory to argue that when thefundamental 119875 mode and the first harmonic 119878 mode are
2 Advances in Acoustics and Vibration
kTh
cc T
25 3 35 4 45 5 55 6 65 7 75 80
5
10
15
20
25
30
35
40
Figure 1 Symmetric Lamb modes on a steel plate (120581 = 183)showing phase velocity as a function of normalized frequency
nearly degenerate at cutoff a coupling effect can occur at theboundaries Uberall et al [12] hypothesize that ldquoone observesa repulsion phenomenon between neighboring dispersioncurves similar to that encountered in atomic physics forquasidegenerate energy levels of atoms when combining intomoleculesrdquo Prada et al [3] express the same view in thewords ldquothis phenomenon leads to a strong repulsion betweenthe dispersion curves of the neighbouring modesrdquo
It is clear that all of these authors focused on the pairanomaly only because in the 119878
1anomaly the 119878
1mode
remains distinct and it does not coincide with any othermode at cutoff Mode repulsion cannot explain 119878
1anomaly
To the best of our knowledge the 1198781anomaly still remains
an unsolved mystery Recently Hussain and Ahmad [13]considered ZGV points in the spectrum of Lamb modes incompressible orthotropic plate It was found that in additionto modes with a single ZGV point a large number of modesexist with multiple such points
In this paper we will examine Rayleigh-Lamb spectrumfor the symmetric modes of an isotropic material We willanalyze (1) and derive mathematical expressions which willexplain both types of anomalies
2 The Mode Spectrum
Let 119896 and 119888 respectively denote the wave number and phasespeed of the mode Define the dimensionless speed 119888119888
119879by 119910
and the dimensionless frequency 120596ℎ119888119879by 119906
Then
119901ℎ = ℎradic1205962
1198882
119879
minus 1198962
= ℎ119896radic1199102minus 1 =
ℎ119896119888119888119879
119888119888119879
radic1199102minus 1 =
119906
119910
radic1199102minus 1
(4)
119902ℎ =119906
119910
radic1199102
1205812minus 1 (5)
With respect to the variables 119906 and 119910 (1) becomes
119891 (119906 119910)
= (1199102minus 2)2
sin(radic1199102 minus 1119906119910) cos(radic
1199102
1205812minus 1
119906
119910)
+ 4radic1199102minus 1radic
1199102
1205812minus 1 sin(radic
1199102
1205812minus 1
119906
119910)
times cos(radic1199102 minus 1119906119910) = 0
(6)
In this section we will consider 120581 = 2 We will calculatethe derivative 119889119910119889119906 at two positions of the spectrum Wewrite
119863119899120581=119889119910
119889119906
10038161003816100381610038161003816100381610038161003816119906=119906119899119910=120581
119863119899119871=119889119910
119889119906
10038161003816100381610038161003816100381610038161003816119906=119906119899119910=119871≫120581
(7)
where the subscript 119899 refers to themode under considerationFor 2radic3 lt 120581 lt 339 (minus1 lt ] lt 0452) we will show that119863119899120581lt 0 for all modes On the other hand119863
1119871gt 0 for the 119878
1
mode while119863119899119871lt 0 for all other modes Since the derivative
for the 1198781mode changes from positive to negative it must
exhibit a bulge before 119910 = 120581 No other mode undergoes areversal of the slope hence all other modes continue theirdownward journey until they asymptotically approach theline 119910 = 1
In Appendix A we give expressions for 120597119891120597119906 and 120597119891120597119910The derivative 119889119910119889119906 is found as
119889119910
119889119906= minus
120597119891120597119906
120597119891120597119910 (8)
When 119910 = 120581 (6) becomes
sin(119906radic1205812minus 1
120581) = 0 (9)
Therefore
119906119899=
119899120587120581
radic1205812minus 1
(10)
Equation (10) shows that the line 119910 = 120581 intersects themodes at infinitely many points At 119910 = 120581 and 119906 = 119906
119899 partial
derivatives (A1) become
120597119891
120597119906
10038161003816100381610038161003816100381610038161003816119906=119906119899119910=120581
=
(1205812minus 2)2radic1205812minus 1
120581
120597119891
120597119910
10038161003816100381610038161003816100381610038161003816119906=119906119899119910=120581
= [
[
(1205812minus 2)2
1205812radic1205812minus 1
+ 4
radic1205812minus 1
1205812
]
]
119906119899
(11)
Advances in Acoustics and Vibration 3
Hence
119863119899120581= minus
(1205812minus 1)32
(1205812minus 2)2
[(1205812minus 2)2
+ 4 (1205812minus 1)] 119899120587
(12)
It is clear that119863119899120581lt 0 for all modes Also |119863
119899120581| becomes
progressively smaller as 119899 increases and 119863119899120581
rarr 0 as 119899 rarr
infin This means that for 119910 = 120581 there is a plateau region andthis plateau is flatter for higher modes
Next we find 119863119899119871 For 119910 ≫ 120581 the expressions for 120597119891120597119906
and 120597119891120597119910 are given by
120597119891
120597119906≃ 1199104[cos 119906 cos 119906
120581minus1
120581sin 119906 sin 119906
120581] (13)
120597119891
120597119910≃ 119906119910 cos 119906 cos 119906
120581+ 41199103 cos 119906
120581sin 119906
+8119910
120581cos 119906 sin 119906
120581minus 120581119906119910 sin 119906 sin 119906
120581
(14)
Thus
119889119910
119889119906
≃ minus
1199104minus (1199104120581) tan 119906 tan (119906120581)
119906119910 + 41199103 tan 119906 + (8119910120581) tan (119906120581) minus 120581119906119910 tan 119906 tan (119906120581)
(15)
For 119910 ≫ 120581 (6) gives
1199102≃ minus
4 tan (119906120581)120581 tan 119906
(16)
Also from (15) and (16) we have
119863119899119871≃ minus
1199103+ (11991054) tan2119906
119899
119906119899+ 1199102 tan 119906
119899(2 + (120581
24) 119906119899tan 119906119899) (17)
or equivalently
119863119899119871≃ minus
1199103+ (11991054) tan2119906
119899
119906119899minus (4120581) tan (119906
119899120581) (2 + (120581
24) 119906119899tan 119906119899) (18)
We have replaced 119906 by 119906119899in (17) and (18) since for a fixed
119910 (16) yields infinitely many roots 119906119899 119899 = 1 2 3
To fix ideas we consider the case of a steel plate for which120581 = 183 The general case follows on similar lines
From (16) we see that for the 1198781mode 119906
1120581 should be
slightly less than 1205872 so that 1199061120581 is in the first quadrant and
the corresponding 1199061is in the second quadrant to yield a large
positive 1199102Hence for the mode 119878
1 we have
1198631119871
≃ minus
1199103+ (11991054) tan2 (1205811205872)
(1205811205872) + 1199102 tan (1205811205872) (2 + (12058124) sdot (1205811205872) tan (1205811205872))
(19)
For 120581 = 183 and for large 119910 1198631119871gt 0
Table 1 Approximate and exact values of 119906119899when 119910 = 20 for the
first five modes
Modes Approximate 119906119899
Exact value at 119910 = 201198781
2875 28561198782
3142 31801198783
6283 62891198784
8624 86501198785
9425 9449
For 2radic3 lt 120581 lt 2 and large 119910 approximate values of 119906119899
from (16) for the first few modes are 1205811205872 120587 31205811205872 2120587 and51205811205872 For the steel plate these values are compared inTable 1with the exact values found from (6) when 119910 = 20
We have seen previously that 1198631119871
gt 0 for the 1198781mode
Now for the 1198782mode 119906
2≃ 120587 and from (18) we get
1198632119871≃ minus
1199103
120587 minus (8120581) tan (120587120581) (20)
Here 120581 = 183 and tan(120587120581) lt 0 thus 1198632119871
lt 0 Ina similar fashion by successively using (17) and (18) we canshow that119863
119899119871lt 0 for all 119899 ge 2
From the previous we conclude that for steel the 1198781is the
only mode which reverses its slope while going from largevalues of 119910 to 119910 = 120581 The previous analysis applies to allmaterials with 120581 lt 2
If 120581 gt 2 the 1198781mode occurs when 119906
1≃ 120587 and from (18)
the 1198781mode will have positive slope as long as
120587 minus8
120581tan 120587
120581lt 0 (21)
or 2 lt 120581 lt 339 which corresponds to 13 lt ] lt 0452Thus we have established that the 119878
1mode will be
anomalous for all materials falling in the range 2radic3 lt 120581 lt339 Since the slope of 119878
1becomes negative for all 119910 when
120581 gt 339 the mode will lose its anomalous character beyond120581 = 339 which corresponds to ] = 0452
3 The Exceptional Case 120581 = 2
The case 120581 = 2 merits special treatment The spectrum ofsymmetric modes appears as in Figure 2
The pairs 1198781-1198782 1198784-1198785 1198787-1198788 appear to merge for large
119910 and then bifurcate as they descend to lower values ofthe phase speed On the other hand 119878
3 1198786 1198789 appear to
behave normallyThis phenomenon was first reported by Mindlin [14]
Each of the modes 1198781 1198784 1198787 shows anomalous dispersion
With 120581 = 2 (6) becomes for 119910 ≫ 1
1199104 cos 119906
2sin 119906 + 1199102 sin 119906
2cos 119906 = 0 (22)
which is satisfied for 119906119899= 2119899120587 119899 = 1 2 3 It is shown in
Appendix B that a more accurate solution of (6) is
119906119899= 119899120587(2 +
1
1199102) (23)
4 Advances in Acoustics and Vibration
0 2 4 6 8 10 12 14 16 18 200
5
10
15
20
25
kTh
cc T
Figure 2 Symmetric Lamb modes on a nickel plate (120581 = 2)
In addition to (23) (16) has roots given by
minus1
21199102≃tan (1199062)tan 119906
=1
2(1 minus tan2 119906
2) (24)
Ignoring 1 in comparison with 1199102 we get
tan2 1199062≃ 1199102 (25)
or
cot2 1199062≃1
1199102 (26)
Let
119906
2=(2119899 + 1) 120587
2+ 120598 (27)
Equation (26) becomes
cot2 (1205872+ 120598) ≃
1
1199102 (28)
or
tan2120598 ≃ 1
1199102 (29)
which leads to
120598 ≃ plusmn1
119910 (30)
Thus for large 119910 1199061= 120587 minus 2120598 119906
2= 120587 + 2120598 119906
4= 3120587 minus 2120598
1199065= 3120587 + 2120598 and so forthSince 120598 rarr 0 as 119910 rarr infin the modes 119906
1 1199062 1199064 1199065
1199067 1199068 appear to coalesce for large 119910 Now with 120581 = 2 (18)
gives 1198631119871
gt 0 1198634119871
gt 0 and 1198637119871
gt 0 while the slopes forall other modes are negative This argument establishes theanomalous dispersion of the modes 119878
3119899+1 119899 = 0 1 2 3 As
1199063 1199066 1199069 occur slightly above 2120587 4120587 6120587 (17) gives a
negative value for the slope of each of these modes Hencethese modes behave in a normal manner
4 Conclusion
We have explained analytically the anomalous behavior ofLamb modes for an isotropic material by looking at the slopeof each mode for large as well as small 119910 For small 119910 slope isfound at 119910 = 120581 This simple technique explains in an analyticmanner theoretical results given by several authors about theanomalous dispersion of the 119878
1mode
Appendices
A The Partial Derivatives
Expressions for the partial derivatives are as follows
120597119891
120597119906
= ((1199102minus 2)2
radic1199102minus 1 cos
119906radic1199102minus 1
119910
times cos119906radic11991021205812minus 1
119910)(119910)
minus1
+(4(1199102
1205812minus 1)radic119910
2minus 1 cos
119906radic1199102minus 1
119910
times cos119906radic11991021205812minus 1
119910)(119910)
minus1
minus((1199102minus 2)2radic1199102
1205812minus 1 sin
119906radic1199102minus 1
119910
times sin119906radic11991021205812minus 1
119910)(119910)
minus1
minus(4 (1199102minus 1)radic
1199102
1205812minus 1 sin
119906radic1199102minus 1
119910
times sin119906radic11991021205812minus 1
119910)(119910)
minus1
120597119891
120597119910
= (1199102minus 2)2
(119906
radic1199102minus 1
minus
119906radic1199102minus 1
1199102
)
Advances in Acoustics and Vibration 5
times cos119906radic1199102minus 1
119910cos
119906radic11991021205812minus 1
119910
+ 4radic1199102minus 1radic119910
21205812minus 1
times(119906
1205812radic11991021205812minus 1
minus
119906radic11991021205812minus 1
1199102
)
times cos119906radic1199102minus 1
119910cos
119906radic11991021205812minus 1
119910
+ 4119910 (1199102minus 2) sin
119906radic1199102minus 1
119910cos
119906radic11991021205812minus 1
119910
+(4119910radic1199102minus 1 cos
119906radic1199102minus 1
119910
times sin119906radic11991021205812minus 1
119910)(1205812radic11991021205812minus 1)
minus1
+(4119910radic11991021205812minus 1 cos
119906radic1199102minus 1
119910
times sin119906radic11991021205812minus 1
119910)(radic119910
2minus 1)
minus1
minus 4radic1199102minus 1radic119910
21205812minus 1(
119906
radic1199102minus 1
minus
119906radic1199102minus 1
1199102
)
times sin119906radic1199102minus 1
119910sin
119906radic11991021205812minus 1
119910
minus (1199102minus 2)2
(119906
1205812radic11991021205812minus 1
minus
119906radic11991021205812minus 1
1199102
)
times sin119906radic1199102minus 1
119910sin
119906radic11991021205812minus 1
119910
(A1)
B The Mode 1198783119899
for 120581 = 2
For 119910 ≫ 1 radic1199102 minus 1119910 ≃ 1 minus 1(21199102) and radic(11991024) minus 1119910 ≃12 minus 1119910
2
Let 119906119899≃ 2119899120587+(120572
1198991199102) and ignore the terms of order 11199104
or higher Then
cos(radic1199102minus 1
119910119906119899) ≃ 1
cos(radic11991024 minus 1
119910119906119899) ≃ minus1
sin(radic1199102minus 1
119910119906119899) ≃ sin
120572119899minus 119899120587
1199102
≃120572119899minus 119899120587
1199102
sin(radic11991024 minus 1
119910119906119899) ≃ ∓ sin
120572119899minus 2119899120587
1199102
≃ ∓120572119899minus 2119899120587
1199102
(B1)
Putting these expressions in (6) we have
minus1199104120572119899 minus 119899120587
1199102
∓ 2 (120572119899minus 2119899120587) = 0 (B2)
or
(1199102plusmn 2) 120572
119899= 119899120587119910
2∓ 4119899120587 (B3)
or
120572119899=1198991205871199102∓ 4119899120587
1199102plusmn 2
≃ 119899120587 (B4)
for large 119910This result shows that the modes 119878
3119899 119899 = 1 2 3
intersect the line 119910 = 1199100 for large 119910
0 at points slightly to
the right of 119906119899= 2119899120587 119899 = 1 2 3
Acknowledgment
Faiz Ahmad is grateful to the Higher Education Commissionof Pakistan for financial support
References
[1] J D Achenbach Wave Propagation in Elastic Solids chapter 6North-Holland Amsterdam The Netherlands 1980
[2] A H Meitzler ldquoBackward wave tranmission stress pulses inelstic cylinders and platesrdquo Journal of the Acoustical Society ofAmerica vol 38 pp 835ndash842 1965
[3] C Prada D Clorennec and D Royer ldquoLocal vibration of anelastic plate and zero-group velocity Lamb modesrdquo Journal ofthe Acoustical Society of America vol 124 no 1 pp 203ndash2122008
[4] K Nishimiya K Mizutani N Wakatsuki and K YamamotoldquoDetermination of 12 condition for fastest NGV of Lamb-Typewaves under each density ratio of solid and liquid layersrdquoAcoustics 08 Paris pp 3613ndash3618
6 Advances in Acoustics and Vibration
[5] J Wolf T D K Nook R Kille andW G Mayer ldquoInvestigationof lamb waves having negative group velocityrdquo Journal of theAcoustical Society of America vol 83 pp 122ndash126 1988
[6] O Balogun T W Murray and C Prada ldquoSimulation andmeasurement of the optical excitation of the S1 zero groupvelocity Lamb wave resonance in platesrdquo Journal of AppliedPhysics vol 102 no 6 Article ID 064914 2007
[7] K Negishi ldquoNegative group velocities of Lamb wavesrdquo Journalof the Acoustical Society of America vol 64 no 1 p S63 1978
[8] M Germano A Alippi A Bettucci and G Mancuso ldquoAnoma-lous and negative reflection of Lamb waves in mode conver-sionrdquo Physical Review B vol 85 no 1 Article ID 012102 2012
[9] I Tolstoy and E Usdin ldquoWave propagation in elastic plates lowand high mode dispersionrdquo Journal of the Acoustical Society ofAmerica vol 29 pp 37ndash42 1957
[10] M F Werby and H Uberall ldquoThe analysis and interpretation ofsome special properties of higher order symmetric Lambwavesthe case for platesrdquo Journal of the Acoustical Society of Americavol 111 no 6 pp 2686ndash2691 2002
[11] N A Whitaker Jr and H A Haus ldquoBackward wave effectin acoustic scattering measurementsrdquo IEEE Ultrasonics Sympo-sium pp 891ndash894 1983
[12] H Uberall B Hosten M Deschamps and A Gerard ldquoRepul-sion of phase-velocity dispersion curves and the nature of platevibrationsrdquo Journal of the Acoustical Society of America vol 96no 2 pp 908ndash917 1994
[13] T Hussain and F Ahmad ldquoLamb modes with multiple zero-group velocity points in an orthotropic platerdquo Journal of theAcoustical Society of America vol 32 pp 641ndash645 2012
[14] R D Mindlin An Introduction To the Mathematical Theory ofVibrations of Elastic Plates Monograph Sec 211 US ArmySignal Corps Eng Lab Ft Monmouth NJ USA 1995 Editedby J Yang World Scientific Singapore 2006
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2 Advances in Acoustics and Vibration
kTh
cc T
25 3 35 4 45 5 55 6 65 7 75 80
5
10
15
20
25
30
35
40
Figure 1 Symmetric Lamb modes on a steel plate (120581 = 183)showing phase velocity as a function of normalized frequency
nearly degenerate at cutoff a coupling effect can occur at theboundaries Uberall et al [12] hypothesize that ldquoone observesa repulsion phenomenon between neighboring dispersioncurves similar to that encountered in atomic physics forquasidegenerate energy levels of atoms when combining intomoleculesrdquo Prada et al [3] express the same view in thewords ldquothis phenomenon leads to a strong repulsion betweenthe dispersion curves of the neighbouring modesrdquo
It is clear that all of these authors focused on the pairanomaly only because in the 119878
1anomaly the 119878
1mode
remains distinct and it does not coincide with any othermode at cutoff Mode repulsion cannot explain 119878
1anomaly
To the best of our knowledge the 1198781anomaly still remains
an unsolved mystery Recently Hussain and Ahmad [13]considered ZGV points in the spectrum of Lamb modes incompressible orthotropic plate It was found that in additionto modes with a single ZGV point a large number of modesexist with multiple such points
In this paper we will examine Rayleigh-Lamb spectrumfor the symmetric modes of an isotropic material We willanalyze (1) and derive mathematical expressions which willexplain both types of anomalies
2 The Mode Spectrum
Let 119896 and 119888 respectively denote the wave number and phasespeed of the mode Define the dimensionless speed 119888119888
119879by 119910
and the dimensionless frequency 120596ℎ119888119879by 119906
Then
119901ℎ = ℎradic1205962
1198882
119879
minus 1198962
= ℎ119896radic1199102minus 1 =
ℎ119896119888119888119879
119888119888119879
radic1199102minus 1 =
119906
119910
radic1199102minus 1
(4)
119902ℎ =119906
119910
radic1199102
1205812minus 1 (5)
With respect to the variables 119906 and 119910 (1) becomes
119891 (119906 119910)
= (1199102minus 2)2
sin(radic1199102 minus 1119906119910) cos(radic
1199102
1205812minus 1
119906
119910)
+ 4radic1199102minus 1radic
1199102
1205812minus 1 sin(radic
1199102
1205812minus 1
119906
119910)
times cos(radic1199102 minus 1119906119910) = 0
(6)
In this section we will consider 120581 = 2 We will calculatethe derivative 119889119910119889119906 at two positions of the spectrum Wewrite
119863119899120581=119889119910
119889119906
10038161003816100381610038161003816100381610038161003816119906=119906119899119910=120581
119863119899119871=119889119910
119889119906
10038161003816100381610038161003816100381610038161003816119906=119906119899119910=119871≫120581
(7)
where the subscript 119899 refers to themode under considerationFor 2radic3 lt 120581 lt 339 (minus1 lt ] lt 0452) we will show that119863119899120581lt 0 for all modes On the other hand119863
1119871gt 0 for the 119878
1
mode while119863119899119871lt 0 for all other modes Since the derivative
for the 1198781mode changes from positive to negative it must
exhibit a bulge before 119910 = 120581 No other mode undergoes areversal of the slope hence all other modes continue theirdownward journey until they asymptotically approach theline 119910 = 1
In Appendix A we give expressions for 120597119891120597119906 and 120597119891120597119910The derivative 119889119910119889119906 is found as
119889119910
119889119906= minus
120597119891120597119906
120597119891120597119910 (8)
When 119910 = 120581 (6) becomes
sin(119906radic1205812minus 1
120581) = 0 (9)
Therefore
119906119899=
119899120587120581
radic1205812minus 1
(10)
Equation (10) shows that the line 119910 = 120581 intersects themodes at infinitely many points At 119910 = 120581 and 119906 = 119906
119899 partial
derivatives (A1) become
120597119891
120597119906
10038161003816100381610038161003816100381610038161003816119906=119906119899119910=120581
=
(1205812minus 2)2radic1205812minus 1
120581
120597119891
120597119910
10038161003816100381610038161003816100381610038161003816119906=119906119899119910=120581
= [
[
(1205812minus 2)2
1205812radic1205812minus 1
+ 4
radic1205812minus 1
1205812
]
]
119906119899
(11)
Advances in Acoustics and Vibration 3
Hence
119863119899120581= minus
(1205812minus 1)32
(1205812minus 2)2
[(1205812minus 2)2
+ 4 (1205812minus 1)] 119899120587
(12)
It is clear that119863119899120581lt 0 for all modes Also |119863
119899120581| becomes
progressively smaller as 119899 increases and 119863119899120581
rarr 0 as 119899 rarr
infin This means that for 119910 = 120581 there is a plateau region andthis plateau is flatter for higher modes
Next we find 119863119899119871 For 119910 ≫ 120581 the expressions for 120597119891120597119906
and 120597119891120597119910 are given by
120597119891
120597119906≃ 1199104[cos 119906 cos 119906
120581minus1
120581sin 119906 sin 119906
120581] (13)
120597119891
120597119910≃ 119906119910 cos 119906 cos 119906
120581+ 41199103 cos 119906
120581sin 119906
+8119910
120581cos 119906 sin 119906
120581minus 120581119906119910 sin 119906 sin 119906
120581
(14)
Thus
119889119910
119889119906
≃ minus
1199104minus (1199104120581) tan 119906 tan (119906120581)
119906119910 + 41199103 tan 119906 + (8119910120581) tan (119906120581) minus 120581119906119910 tan 119906 tan (119906120581)
(15)
For 119910 ≫ 120581 (6) gives
1199102≃ minus
4 tan (119906120581)120581 tan 119906
(16)
Also from (15) and (16) we have
119863119899119871≃ minus
1199103+ (11991054) tan2119906
119899
119906119899+ 1199102 tan 119906
119899(2 + (120581
24) 119906119899tan 119906119899) (17)
or equivalently
119863119899119871≃ minus
1199103+ (11991054) tan2119906
119899
119906119899minus (4120581) tan (119906
119899120581) (2 + (120581
24) 119906119899tan 119906119899) (18)
We have replaced 119906 by 119906119899in (17) and (18) since for a fixed
119910 (16) yields infinitely many roots 119906119899 119899 = 1 2 3
To fix ideas we consider the case of a steel plate for which120581 = 183 The general case follows on similar lines
From (16) we see that for the 1198781mode 119906
1120581 should be
slightly less than 1205872 so that 1199061120581 is in the first quadrant and
the corresponding 1199061is in the second quadrant to yield a large
positive 1199102Hence for the mode 119878
1 we have
1198631119871
≃ minus
1199103+ (11991054) tan2 (1205811205872)
(1205811205872) + 1199102 tan (1205811205872) (2 + (12058124) sdot (1205811205872) tan (1205811205872))
(19)
For 120581 = 183 and for large 119910 1198631119871gt 0
Table 1 Approximate and exact values of 119906119899when 119910 = 20 for the
first five modes
Modes Approximate 119906119899
Exact value at 119910 = 201198781
2875 28561198782
3142 31801198783
6283 62891198784
8624 86501198785
9425 9449
For 2radic3 lt 120581 lt 2 and large 119910 approximate values of 119906119899
from (16) for the first few modes are 1205811205872 120587 31205811205872 2120587 and51205811205872 For the steel plate these values are compared inTable 1with the exact values found from (6) when 119910 = 20
We have seen previously that 1198631119871
gt 0 for the 1198781mode
Now for the 1198782mode 119906
2≃ 120587 and from (18) we get
1198632119871≃ minus
1199103
120587 minus (8120581) tan (120587120581) (20)
Here 120581 = 183 and tan(120587120581) lt 0 thus 1198632119871
lt 0 Ina similar fashion by successively using (17) and (18) we canshow that119863
119899119871lt 0 for all 119899 ge 2
From the previous we conclude that for steel the 1198781is the
only mode which reverses its slope while going from largevalues of 119910 to 119910 = 120581 The previous analysis applies to allmaterials with 120581 lt 2
If 120581 gt 2 the 1198781mode occurs when 119906
1≃ 120587 and from (18)
the 1198781mode will have positive slope as long as
120587 minus8
120581tan 120587
120581lt 0 (21)
or 2 lt 120581 lt 339 which corresponds to 13 lt ] lt 0452Thus we have established that the 119878
1mode will be
anomalous for all materials falling in the range 2radic3 lt 120581 lt339 Since the slope of 119878
1becomes negative for all 119910 when
120581 gt 339 the mode will lose its anomalous character beyond120581 = 339 which corresponds to ] = 0452
3 The Exceptional Case 120581 = 2
The case 120581 = 2 merits special treatment The spectrum ofsymmetric modes appears as in Figure 2
The pairs 1198781-1198782 1198784-1198785 1198787-1198788 appear to merge for large
119910 and then bifurcate as they descend to lower values ofthe phase speed On the other hand 119878
3 1198786 1198789 appear to
behave normallyThis phenomenon was first reported by Mindlin [14]
Each of the modes 1198781 1198784 1198787 shows anomalous dispersion
With 120581 = 2 (6) becomes for 119910 ≫ 1
1199104 cos 119906
2sin 119906 + 1199102 sin 119906
2cos 119906 = 0 (22)
which is satisfied for 119906119899= 2119899120587 119899 = 1 2 3 It is shown in
Appendix B that a more accurate solution of (6) is
119906119899= 119899120587(2 +
1
1199102) (23)
4 Advances in Acoustics and Vibration
0 2 4 6 8 10 12 14 16 18 200
5
10
15
20
25
kTh
cc T
Figure 2 Symmetric Lamb modes on a nickel plate (120581 = 2)
In addition to (23) (16) has roots given by
minus1
21199102≃tan (1199062)tan 119906
=1
2(1 minus tan2 119906
2) (24)
Ignoring 1 in comparison with 1199102 we get
tan2 1199062≃ 1199102 (25)
or
cot2 1199062≃1
1199102 (26)
Let
119906
2=(2119899 + 1) 120587
2+ 120598 (27)
Equation (26) becomes
cot2 (1205872+ 120598) ≃
1
1199102 (28)
or
tan2120598 ≃ 1
1199102 (29)
which leads to
120598 ≃ plusmn1
119910 (30)
Thus for large 119910 1199061= 120587 minus 2120598 119906
2= 120587 + 2120598 119906
4= 3120587 minus 2120598
1199065= 3120587 + 2120598 and so forthSince 120598 rarr 0 as 119910 rarr infin the modes 119906
1 1199062 1199064 1199065
1199067 1199068 appear to coalesce for large 119910 Now with 120581 = 2 (18)
gives 1198631119871
gt 0 1198634119871
gt 0 and 1198637119871
gt 0 while the slopes forall other modes are negative This argument establishes theanomalous dispersion of the modes 119878
3119899+1 119899 = 0 1 2 3 As
1199063 1199066 1199069 occur slightly above 2120587 4120587 6120587 (17) gives a
negative value for the slope of each of these modes Hencethese modes behave in a normal manner
4 Conclusion
We have explained analytically the anomalous behavior ofLamb modes for an isotropic material by looking at the slopeof each mode for large as well as small 119910 For small 119910 slope isfound at 119910 = 120581 This simple technique explains in an analyticmanner theoretical results given by several authors about theanomalous dispersion of the 119878
1mode
Appendices
A The Partial Derivatives
Expressions for the partial derivatives are as follows
120597119891
120597119906
= ((1199102minus 2)2
radic1199102minus 1 cos
119906radic1199102minus 1
119910
times cos119906radic11991021205812minus 1
119910)(119910)
minus1
+(4(1199102
1205812minus 1)radic119910
2minus 1 cos
119906radic1199102minus 1
119910
times cos119906radic11991021205812minus 1
119910)(119910)
minus1
minus((1199102minus 2)2radic1199102
1205812minus 1 sin
119906radic1199102minus 1
119910
times sin119906radic11991021205812minus 1
119910)(119910)
minus1
minus(4 (1199102minus 1)radic
1199102
1205812minus 1 sin
119906radic1199102minus 1
119910
times sin119906radic11991021205812minus 1
119910)(119910)
minus1
120597119891
120597119910
= (1199102minus 2)2
(119906
radic1199102minus 1
minus
119906radic1199102minus 1
1199102
)
Advances in Acoustics and Vibration 5
times cos119906radic1199102minus 1
119910cos
119906radic11991021205812minus 1
119910
+ 4radic1199102minus 1radic119910
21205812minus 1
times(119906
1205812radic11991021205812minus 1
minus
119906radic11991021205812minus 1
1199102
)
times cos119906radic1199102minus 1
119910cos
119906radic11991021205812minus 1
119910
+ 4119910 (1199102minus 2) sin
119906radic1199102minus 1
119910cos
119906radic11991021205812minus 1
119910
+(4119910radic1199102minus 1 cos
119906radic1199102minus 1
119910
times sin119906radic11991021205812minus 1
119910)(1205812radic11991021205812minus 1)
minus1
+(4119910radic11991021205812minus 1 cos
119906radic1199102minus 1
119910
times sin119906radic11991021205812minus 1
119910)(radic119910
2minus 1)
minus1
minus 4radic1199102minus 1radic119910
21205812minus 1(
119906
radic1199102minus 1
minus
119906radic1199102minus 1
1199102
)
times sin119906radic1199102minus 1
119910sin
119906radic11991021205812minus 1
119910
minus (1199102minus 2)2
(119906
1205812radic11991021205812minus 1
minus
119906radic11991021205812minus 1
1199102
)
times sin119906radic1199102minus 1
119910sin
119906radic11991021205812minus 1
119910
(A1)
B The Mode 1198783119899
for 120581 = 2
For 119910 ≫ 1 radic1199102 minus 1119910 ≃ 1 minus 1(21199102) and radic(11991024) minus 1119910 ≃12 minus 1119910
2
Let 119906119899≃ 2119899120587+(120572
1198991199102) and ignore the terms of order 11199104
or higher Then
cos(radic1199102minus 1
119910119906119899) ≃ 1
cos(radic11991024 minus 1
119910119906119899) ≃ minus1
sin(radic1199102minus 1
119910119906119899) ≃ sin
120572119899minus 119899120587
1199102
≃120572119899minus 119899120587
1199102
sin(radic11991024 minus 1
119910119906119899) ≃ ∓ sin
120572119899minus 2119899120587
1199102
≃ ∓120572119899minus 2119899120587
1199102
(B1)
Putting these expressions in (6) we have
minus1199104120572119899 minus 119899120587
1199102
∓ 2 (120572119899minus 2119899120587) = 0 (B2)
or
(1199102plusmn 2) 120572
119899= 119899120587119910
2∓ 4119899120587 (B3)
or
120572119899=1198991205871199102∓ 4119899120587
1199102plusmn 2
≃ 119899120587 (B4)
for large 119910This result shows that the modes 119878
3119899 119899 = 1 2 3
intersect the line 119910 = 1199100 for large 119910
0 at points slightly to
the right of 119906119899= 2119899120587 119899 = 1 2 3
Acknowledgment
Faiz Ahmad is grateful to the Higher Education Commissionof Pakistan for financial support
References
[1] J D Achenbach Wave Propagation in Elastic Solids chapter 6North-Holland Amsterdam The Netherlands 1980
[2] A H Meitzler ldquoBackward wave tranmission stress pulses inelstic cylinders and platesrdquo Journal of the Acoustical Society ofAmerica vol 38 pp 835ndash842 1965
[3] C Prada D Clorennec and D Royer ldquoLocal vibration of anelastic plate and zero-group velocity Lamb modesrdquo Journal ofthe Acoustical Society of America vol 124 no 1 pp 203ndash2122008
[4] K Nishimiya K Mizutani N Wakatsuki and K YamamotoldquoDetermination of 12 condition for fastest NGV of Lamb-Typewaves under each density ratio of solid and liquid layersrdquoAcoustics 08 Paris pp 3613ndash3618
6 Advances in Acoustics and Vibration
[5] J Wolf T D K Nook R Kille andW G Mayer ldquoInvestigationof lamb waves having negative group velocityrdquo Journal of theAcoustical Society of America vol 83 pp 122ndash126 1988
[6] O Balogun T W Murray and C Prada ldquoSimulation andmeasurement of the optical excitation of the S1 zero groupvelocity Lamb wave resonance in platesrdquo Journal of AppliedPhysics vol 102 no 6 Article ID 064914 2007
[7] K Negishi ldquoNegative group velocities of Lamb wavesrdquo Journalof the Acoustical Society of America vol 64 no 1 p S63 1978
[8] M Germano A Alippi A Bettucci and G Mancuso ldquoAnoma-lous and negative reflection of Lamb waves in mode conver-sionrdquo Physical Review B vol 85 no 1 Article ID 012102 2012
[9] I Tolstoy and E Usdin ldquoWave propagation in elastic plates lowand high mode dispersionrdquo Journal of the Acoustical Society ofAmerica vol 29 pp 37ndash42 1957
[10] M F Werby and H Uberall ldquoThe analysis and interpretation ofsome special properties of higher order symmetric Lambwavesthe case for platesrdquo Journal of the Acoustical Society of Americavol 111 no 6 pp 2686ndash2691 2002
[11] N A Whitaker Jr and H A Haus ldquoBackward wave effectin acoustic scattering measurementsrdquo IEEE Ultrasonics Sympo-sium pp 891ndash894 1983
[12] H Uberall B Hosten M Deschamps and A Gerard ldquoRepul-sion of phase-velocity dispersion curves and the nature of platevibrationsrdquo Journal of the Acoustical Society of America vol 96no 2 pp 908ndash917 1994
[13] T Hussain and F Ahmad ldquoLamb modes with multiple zero-group velocity points in an orthotropic platerdquo Journal of theAcoustical Society of America vol 32 pp 641ndash645 2012
[14] R D Mindlin An Introduction To the Mathematical Theory ofVibrations of Elastic Plates Monograph Sec 211 US ArmySignal Corps Eng Lab Ft Monmouth NJ USA 1995 Editedby J Yang World Scientific Singapore 2006
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International Journal of
Advances in Acoustics and Vibration 3
Hence
119863119899120581= minus
(1205812minus 1)32
(1205812minus 2)2
[(1205812minus 2)2
+ 4 (1205812minus 1)] 119899120587
(12)
It is clear that119863119899120581lt 0 for all modes Also |119863
119899120581| becomes
progressively smaller as 119899 increases and 119863119899120581
rarr 0 as 119899 rarr
infin This means that for 119910 = 120581 there is a plateau region andthis plateau is flatter for higher modes
Next we find 119863119899119871 For 119910 ≫ 120581 the expressions for 120597119891120597119906
and 120597119891120597119910 are given by
120597119891
120597119906≃ 1199104[cos 119906 cos 119906
120581minus1
120581sin 119906 sin 119906
120581] (13)
120597119891
120597119910≃ 119906119910 cos 119906 cos 119906
120581+ 41199103 cos 119906
120581sin 119906
+8119910
120581cos 119906 sin 119906
120581minus 120581119906119910 sin 119906 sin 119906
120581
(14)
Thus
119889119910
119889119906
≃ minus
1199104minus (1199104120581) tan 119906 tan (119906120581)
119906119910 + 41199103 tan 119906 + (8119910120581) tan (119906120581) minus 120581119906119910 tan 119906 tan (119906120581)
(15)
For 119910 ≫ 120581 (6) gives
1199102≃ minus
4 tan (119906120581)120581 tan 119906
(16)
Also from (15) and (16) we have
119863119899119871≃ minus
1199103+ (11991054) tan2119906
119899
119906119899+ 1199102 tan 119906
119899(2 + (120581
24) 119906119899tan 119906119899) (17)
or equivalently
119863119899119871≃ minus
1199103+ (11991054) tan2119906
119899
119906119899minus (4120581) tan (119906
119899120581) (2 + (120581
24) 119906119899tan 119906119899) (18)
We have replaced 119906 by 119906119899in (17) and (18) since for a fixed
119910 (16) yields infinitely many roots 119906119899 119899 = 1 2 3
To fix ideas we consider the case of a steel plate for which120581 = 183 The general case follows on similar lines
From (16) we see that for the 1198781mode 119906
1120581 should be
slightly less than 1205872 so that 1199061120581 is in the first quadrant and
the corresponding 1199061is in the second quadrant to yield a large
positive 1199102Hence for the mode 119878
1 we have
1198631119871
≃ minus
1199103+ (11991054) tan2 (1205811205872)
(1205811205872) + 1199102 tan (1205811205872) (2 + (12058124) sdot (1205811205872) tan (1205811205872))
(19)
For 120581 = 183 and for large 119910 1198631119871gt 0
Table 1 Approximate and exact values of 119906119899when 119910 = 20 for the
first five modes
Modes Approximate 119906119899
Exact value at 119910 = 201198781
2875 28561198782
3142 31801198783
6283 62891198784
8624 86501198785
9425 9449
For 2radic3 lt 120581 lt 2 and large 119910 approximate values of 119906119899
from (16) for the first few modes are 1205811205872 120587 31205811205872 2120587 and51205811205872 For the steel plate these values are compared inTable 1with the exact values found from (6) when 119910 = 20
We have seen previously that 1198631119871
gt 0 for the 1198781mode
Now for the 1198782mode 119906
2≃ 120587 and from (18) we get
1198632119871≃ minus
1199103
120587 minus (8120581) tan (120587120581) (20)
Here 120581 = 183 and tan(120587120581) lt 0 thus 1198632119871
lt 0 Ina similar fashion by successively using (17) and (18) we canshow that119863
119899119871lt 0 for all 119899 ge 2
From the previous we conclude that for steel the 1198781is the
only mode which reverses its slope while going from largevalues of 119910 to 119910 = 120581 The previous analysis applies to allmaterials with 120581 lt 2
If 120581 gt 2 the 1198781mode occurs when 119906
1≃ 120587 and from (18)
the 1198781mode will have positive slope as long as
120587 minus8
120581tan 120587
120581lt 0 (21)
or 2 lt 120581 lt 339 which corresponds to 13 lt ] lt 0452Thus we have established that the 119878
1mode will be
anomalous for all materials falling in the range 2radic3 lt 120581 lt339 Since the slope of 119878
1becomes negative for all 119910 when
120581 gt 339 the mode will lose its anomalous character beyond120581 = 339 which corresponds to ] = 0452
3 The Exceptional Case 120581 = 2
The case 120581 = 2 merits special treatment The spectrum ofsymmetric modes appears as in Figure 2
The pairs 1198781-1198782 1198784-1198785 1198787-1198788 appear to merge for large
119910 and then bifurcate as they descend to lower values ofthe phase speed On the other hand 119878
3 1198786 1198789 appear to
behave normallyThis phenomenon was first reported by Mindlin [14]
Each of the modes 1198781 1198784 1198787 shows anomalous dispersion
With 120581 = 2 (6) becomes for 119910 ≫ 1
1199104 cos 119906
2sin 119906 + 1199102 sin 119906
2cos 119906 = 0 (22)
which is satisfied for 119906119899= 2119899120587 119899 = 1 2 3 It is shown in
Appendix B that a more accurate solution of (6) is
119906119899= 119899120587(2 +
1
1199102) (23)
4 Advances in Acoustics and Vibration
0 2 4 6 8 10 12 14 16 18 200
5
10
15
20
25
kTh
cc T
Figure 2 Symmetric Lamb modes on a nickel plate (120581 = 2)
In addition to (23) (16) has roots given by
minus1
21199102≃tan (1199062)tan 119906
=1
2(1 minus tan2 119906
2) (24)
Ignoring 1 in comparison with 1199102 we get
tan2 1199062≃ 1199102 (25)
or
cot2 1199062≃1
1199102 (26)
Let
119906
2=(2119899 + 1) 120587
2+ 120598 (27)
Equation (26) becomes
cot2 (1205872+ 120598) ≃
1
1199102 (28)
or
tan2120598 ≃ 1
1199102 (29)
which leads to
120598 ≃ plusmn1
119910 (30)
Thus for large 119910 1199061= 120587 minus 2120598 119906
2= 120587 + 2120598 119906
4= 3120587 minus 2120598
1199065= 3120587 + 2120598 and so forthSince 120598 rarr 0 as 119910 rarr infin the modes 119906
1 1199062 1199064 1199065
1199067 1199068 appear to coalesce for large 119910 Now with 120581 = 2 (18)
gives 1198631119871
gt 0 1198634119871
gt 0 and 1198637119871
gt 0 while the slopes forall other modes are negative This argument establishes theanomalous dispersion of the modes 119878
3119899+1 119899 = 0 1 2 3 As
1199063 1199066 1199069 occur slightly above 2120587 4120587 6120587 (17) gives a
negative value for the slope of each of these modes Hencethese modes behave in a normal manner
4 Conclusion
We have explained analytically the anomalous behavior ofLamb modes for an isotropic material by looking at the slopeof each mode for large as well as small 119910 For small 119910 slope isfound at 119910 = 120581 This simple technique explains in an analyticmanner theoretical results given by several authors about theanomalous dispersion of the 119878
1mode
Appendices
A The Partial Derivatives
Expressions for the partial derivatives are as follows
120597119891
120597119906
= ((1199102minus 2)2
radic1199102minus 1 cos
119906radic1199102minus 1
119910
times cos119906radic11991021205812minus 1
119910)(119910)
minus1
+(4(1199102
1205812minus 1)radic119910
2minus 1 cos
119906radic1199102minus 1
119910
times cos119906radic11991021205812minus 1
119910)(119910)
minus1
minus((1199102minus 2)2radic1199102
1205812minus 1 sin
119906radic1199102minus 1
119910
times sin119906radic11991021205812minus 1
119910)(119910)
minus1
minus(4 (1199102minus 1)radic
1199102
1205812minus 1 sin
119906radic1199102minus 1
119910
times sin119906radic11991021205812minus 1
119910)(119910)
minus1
120597119891
120597119910
= (1199102minus 2)2
(119906
radic1199102minus 1
minus
119906radic1199102minus 1
1199102
)
Advances in Acoustics and Vibration 5
times cos119906radic1199102minus 1
119910cos
119906radic11991021205812minus 1
119910
+ 4radic1199102minus 1radic119910
21205812minus 1
times(119906
1205812radic11991021205812minus 1
minus
119906radic11991021205812minus 1
1199102
)
times cos119906radic1199102minus 1
119910cos
119906radic11991021205812minus 1
119910
+ 4119910 (1199102minus 2) sin
119906radic1199102minus 1
119910cos
119906radic11991021205812minus 1
119910
+(4119910radic1199102minus 1 cos
119906radic1199102minus 1
119910
times sin119906radic11991021205812minus 1
119910)(1205812radic11991021205812minus 1)
minus1
+(4119910radic11991021205812minus 1 cos
119906radic1199102minus 1
119910
times sin119906radic11991021205812minus 1
119910)(radic119910
2minus 1)
minus1
minus 4radic1199102minus 1radic119910
21205812minus 1(
119906
radic1199102minus 1
minus
119906radic1199102minus 1
1199102
)
times sin119906radic1199102minus 1
119910sin
119906radic11991021205812minus 1
119910
minus (1199102minus 2)2
(119906
1205812radic11991021205812minus 1
minus
119906radic11991021205812minus 1
1199102
)
times sin119906radic1199102minus 1
119910sin
119906radic11991021205812minus 1
119910
(A1)
B The Mode 1198783119899
for 120581 = 2
For 119910 ≫ 1 radic1199102 minus 1119910 ≃ 1 minus 1(21199102) and radic(11991024) minus 1119910 ≃12 minus 1119910
2
Let 119906119899≃ 2119899120587+(120572
1198991199102) and ignore the terms of order 11199104
or higher Then
cos(radic1199102minus 1
119910119906119899) ≃ 1
cos(radic11991024 minus 1
119910119906119899) ≃ minus1
sin(radic1199102minus 1
119910119906119899) ≃ sin
120572119899minus 119899120587
1199102
≃120572119899minus 119899120587
1199102
sin(radic11991024 minus 1
119910119906119899) ≃ ∓ sin
120572119899minus 2119899120587
1199102
≃ ∓120572119899minus 2119899120587
1199102
(B1)
Putting these expressions in (6) we have
minus1199104120572119899 minus 119899120587
1199102
∓ 2 (120572119899minus 2119899120587) = 0 (B2)
or
(1199102plusmn 2) 120572
119899= 119899120587119910
2∓ 4119899120587 (B3)
or
120572119899=1198991205871199102∓ 4119899120587
1199102plusmn 2
≃ 119899120587 (B4)
for large 119910This result shows that the modes 119878
3119899 119899 = 1 2 3
intersect the line 119910 = 1199100 for large 119910
0 at points slightly to
the right of 119906119899= 2119899120587 119899 = 1 2 3
Acknowledgment
Faiz Ahmad is grateful to the Higher Education Commissionof Pakistan for financial support
References
[1] J D Achenbach Wave Propagation in Elastic Solids chapter 6North-Holland Amsterdam The Netherlands 1980
[2] A H Meitzler ldquoBackward wave tranmission stress pulses inelstic cylinders and platesrdquo Journal of the Acoustical Society ofAmerica vol 38 pp 835ndash842 1965
[3] C Prada D Clorennec and D Royer ldquoLocal vibration of anelastic plate and zero-group velocity Lamb modesrdquo Journal ofthe Acoustical Society of America vol 124 no 1 pp 203ndash2122008
[4] K Nishimiya K Mizutani N Wakatsuki and K YamamotoldquoDetermination of 12 condition for fastest NGV of Lamb-Typewaves under each density ratio of solid and liquid layersrdquoAcoustics 08 Paris pp 3613ndash3618
6 Advances in Acoustics and Vibration
[5] J Wolf T D K Nook R Kille andW G Mayer ldquoInvestigationof lamb waves having negative group velocityrdquo Journal of theAcoustical Society of America vol 83 pp 122ndash126 1988
[6] O Balogun T W Murray and C Prada ldquoSimulation andmeasurement of the optical excitation of the S1 zero groupvelocity Lamb wave resonance in platesrdquo Journal of AppliedPhysics vol 102 no 6 Article ID 064914 2007
[7] K Negishi ldquoNegative group velocities of Lamb wavesrdquo Journalof the Acoustical Society of America vol 64 no 1 p S63 1978
[8] M Germano A Alippi A Bettucci and G Mancuso ldquoAnoma-lous and negative reflection of Lamb waves in mode conver-sionrdquo Physical Review B vol 85 no 1 Article ID 012102 2012
[9] I Tolstoy and E Usdin ldquoWave propagation in elastic plates lowand high mode dispersionrdquo Journal of the Acoustical Society ofAmerica vol 29 pp 37ndash42 1957
[10] M F Werby and H Uberall ldquoThe analysis and interpretation ofsome special properties of higher order symmetric Lambwavesthe case for platesrdquo Journal of the Acoustical Society of Americavol 111 no 6 pp 2686ndash2691 2002
[11] N A Whitaker Jr and H A Haus ldquoBackward wave effectin acoustic scattering measurementsrdquo IEEE Ultrasonics Sympo-sium pp 891ndash894 1983
[12] H Uberall B Hosten M Deschamps and A Gerard ldquoRepul-sion of phase-velocity dispersion curves and the nature of platevibrationsrdquo Journal of the Acoustical Society of America vol 96no 2 pp 908ndash917 1994
[13] T Hussain and F Ahmad ldquoLamb modes with multiple zero-group velocity points in an orthotropic platerdquo Journal of theAcoustical Society of America vol 32 pp 641ndash645 2012
[14] R D Mindlin An Introduction To the Mathematical Theory ofVibrations of Elastic Plates Monograph Sec 211 US ArmySignal Corps Eng Lab Ft Monmouth NJ USA 1995 Editedby J Yang World Scientific Singapore 2006
International Journal of
AerospaceEngineeringHindawi Publishing Corporationhttpwwwhindawicom Volume 2014
RoboticsJournal of
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
Active and Passive Electronic Components
Control Scienceand Engineering
Journal of
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
International Journal of
RotatingMachinery
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
Hindawi Publishing Corporation httpwwwhindawicom
Journal ofEngineeringVolume 2014
Submit your manuscripts athttpwwwhindawicom
VLSI Design
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
Shock and Vibration
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
Civil EngineeringAdvances in
Acoustics and VibrationAdvances in
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
Electrical and Computer Engineering
Journal of
Advances inOptoElectronics
Hindawi Publishing Corporation httpwwwhindawicom
Volume 2014
The Scientific World JournalHindawi Publishing Corporation httpwwwhindawicom Volume 2014
SensorsJournal of
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
Modelling amp Simulation in EngineeringHindawi Publishing Corporation httpwwwhindawicom Volume 2014
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
Chemical EngineeringInternational Journal of Antennas and
Propagation
International Journal of
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
Navigation and Observation
International Journal of
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
DistributedSensor Networks
International Journal of
4 Advances in Acoustics and Vibration
0 2 4 6 8 10 12 14 16 18 200
5
10
15
20
25
kTh
cc T
Figure 2 Symmetric Lamb modes on a nickel plate (120581 = 2)
In addition to (23) (16) has roots given by
minus1
21199102≃tan (1199062)tan 119906
=1
2(1 minus tan2 119906
2) (24)
Ignoring 1 in comparison with 1199102 we get
tan2 1199062≃ 1199102 (25)
or
cot2 1199062≃1
1199102 (26)
Let
119906
2=(2119899 + 1) 120587
2+ 120598 (27)
Equation (26) becomes
cot2 (1205872+ 120598) ≃
1
1199102 (28)
or
tan2120598 ≃ 1
1199102 (29)
which leads to
120598 ≃ plusmn1
119910 (30)
Thus for large 119910 1199061= 120587 minus 2120598 119906
2= 120587 + 2120598 119906
4= 3120587 minus 2120598
1199065= 3120587 + 2120598 and so forthSince 120598 rarr 0 as 119910 rarr infin the modes 119906
1 1199062 1199064 1199065
1199067 1199068 appear to coalesce for large 119910 Now with 120581 = 2 (18)
gives 1198631119871
gt 0 1198634119871
gt 0 and 1198637119871
gt 0 while the slopes forall other modes are negative This argument establishes theanomalous dispersion of the modes 119878
3119899+1 119899 = 0 1 2 3 As
1199063 1199066 1199069 occur slightly above 2120587 4120587 6120587 (17) gives a
negative value for the slope of each of these modes Hencethese modes behave in a normal manner
4 Conclusion
We have explained analytically the anomalous behavior ofLamb modes for an isotropic material by looking at the slopeof each mode for large as well as small 119910 For small 119910 slope isfound at 119910 = 120581 This simple technique explains in an analyticmanner theoretical results given by several authors about theanomalous dispersion of the 119878
1mode
Appendices
A The Partial Derivatives
Expressions for the partial derivatives are as follows
120597119891
120597119906
= ((1199102minus 2)2
radic1199102minus 1 cos
119906radic1199102minus 1
119910
times cos119906radic11991021205812minus 1
119910)(119910)
minus1
+(4(1199102
1205812minus 1)radic119910
2minus 1 cos
119906radic1199102minus 1
119910
times cos119906radic11991021205812minus 1
119910)(119910)
minus1
minus((1199102minus 2)2radic1199102
1205812minus 1 sin
119906radic1199102minus 1
119910
times sin119906radic11991021205812minus 1
119910)(119910)
minus1
minus(4 (1199102minus 1)radic
1199102
1205812minus 1 sin
119906radic1199102minus 1
119910
times sin119906radic11991021205812minus 1
119910)(119910)
minus1
120597119891
120597119910
= (1199102minus 2)2
(119906
radic1199102minus 1
minus
119906radic1199102minus 1
1199102
)
Advances in Acoustics and Vibration 5
times cos119906radic1199102minus 1
119910cos
119906radic11991021205812minus 1
119910
+ 4radic1199102minus 1radic119910
21205812minus 1
times(119906
1205812radic11991021205812minus 1
minus
119906radic11991021205812minus 1
1199102
)
times cos119906radic1199102minus 1
119910cos
119906radic11991021205812minus 1
119910
+ 4119910 (1199102minus 2) sin
119906radic1199102minus 1
119910cos
119906radic11991021205812minus 1
119910
+(4119910radic1199102minus 1 cos
119906radic1199102minus 1
119910
times sin119906radic11991021205812minus 1
119910)(1205812radic11991021205812minus 1)
minus1
+(4119910radic11991021205812minus 1 cos
119906radic1199102minus 1
119910
times sin119906radic11991021205812minus 1
119910)(radic119910
2minus 1)
minus1
minus 4radic1199102minus 1radic119910
21205812minus 1(
119906
radic1199102minus 1
minus
119906radic1199102minus 1
1199102
)
times sin119906radic1199102minus 1
119910sin
119906radic11991021205812minus 1
119910
minus (1199102minus 2)2
(119906
1205812radic11991021205812minus 1
minus
119906radic11991021205812minus 1
1199102
)
times sin119906radic1199102minus 1
119910sin
119906radic11991021205812minus 1
119910
(A1)
B The Mode 1198783119899
for 120581 = 2
For 119910 ≫ 1 radic1199102 minus 1119910 ≃ 1 minus 1(21199102) and radic(11991024) minus 1119910 ≃12 minus 1119910
2
Let 119906119899≃ 2119899120587+(120572
1198991199102) and ignore the terms of order 11199104
or higher Then
cos(radic1199102minus 1
119910119906119899) ≃ 1
cos(radic11991024 minus 1
119910119906119899) ≃ minus1
sin(radic1199102minus 1
119910119906119899) ≃ sin
120572119899minus 119899120587
1199102
≃120572119899minus 119899120587
1199102
sin(radic11991024 minus 1
119910119906119899) ≃ ∓ sin
120572119899minus 2119899120587
1199102
≃ ∓120572119899minus 2119899120587
1199102
(B1)
Putting these expressions in (6) we have
minus1199104120572119899 minus 119899120587
1199102
∓ 2 (120572119899minus 2119899120587) = 0 (B2)
or
(1199102plusmn 2) 120572
119899= 119899120587119910
2∓ 4119899120587 (B3)
or
120572119899=1198991205871199102∓ 4119899120587
1199102plusmn 2
≃ 119899120587 (B4)
for large 119910This result shows that the modes 119878
3119899 119899 = 1 2 3
intersect the line 119910 = 1199100 for large 119910
0 at points slightly to
the right of 119906119899= 2119899120587 119899 = 1 2 3
Acknowledgment
Faiz Ahmad is grateful to the Higher Education Commissionof Pakistan for financial support
References
[1] J D Achenbach Wave Propagation in Elastic Solids chapter 6North-Holland Amsterdam The Netherlands 1980
[2] A H Meitzler ldquoBackward wave tranmission stress pulses inelstic cylinders and platesrdquo Journal of the Acoustical Society ofAmerica vol 38 pp 835ndash842 1965
[3] C Prada D Clorennec and D Royer ldquoLocal vibration of anelastic plate and zero-group velocity Lamb modesrdquo Journal ofthe Acoustical Society of America vol 124 no 1 pp 203ndash2122008
[4] K Nishimiya K Mizutani N Wakatsuki and K YamamotoldquoDetermination of 12 condition for fastest NGV of Lamb-Typewaves under each density ratio of solid and liquid layersrdquoAcoustics 08 Paris pp 3613ndash3618
6 Advances in Acoustics and Vibration
[5] J Wolf T D K Nook R Kille andW G Mayer ldquoInvestigationof lamb waves having negative group velocityrdquo Journal of theAcoustical Society of America vol 83 pp 122ndash126 1988
[6] O Balogun T W Murray and C Prada ldquoSimulation andmeasurement of the optical excitation of the S1 zero groupvelocity Lamb wave resonance in platesrdquo Journal of AppliedPhysics vol 102 no 6 Article ID 064914 2007
[7] K Negishi ldquoNegative group velocities of Lamb wavesrdquo Journalof the Acoustical Society of America vol 64 no 1 p S63 1978
[8] M Germano A Alippi A Bettucci and G Mancuso ldquoAnoma-lous and negative reflection of Lamb waves in mode conver-sionrdquo Physical Review B vol 85 no 1 Article ID 012102 2012
[9] I Tolstoy and E Usdin ldquoWave propagation in elastic plates lowand high mode dispersionrdquo Journal of the Acoustical Society ofAmerica vol 29 pp 37ndash42 1957
[10] M F Werby and H Uberall ldquoThe analysis and interpretation ofsome special properties of higher order symmetric Lambwavesthe case for platesrdquo Journal of the Acoustical Society of Americavol 111 no 6 pp 2686ndash2691 2002
[11] N A Whitaker Jr and H A Haus ldquoBackward wave effectin acoustic scattering measurementsrdquo IEEE Ultrasonics Sympo-sium pp 891ndash894 1983
[12] H Uberall B Hosten M Deschamps and A Gerard ldquoRepul-sion of phase-velocity dispersion curves and the nature of platevibrationsrdquo Journal of the Acoustical Society of America vol 96no 2 pp 908ndash917 1994
[13] T Hussain and F Ahmad ldquoLamb modes with multiple zero-group velocity points in an orthotropic platerdquo Journal of theAcoustical Society of America vol 32 pp 641ndash645 2012
[14] R D Mindlin An Introduction To the Mathematical Theory ofVibrations of Elastic Plates Monograph Sec 211 US ArmySignal Corps Eng Lab Ft Monmouth NJ USA 1995 Editedby J Yang World Scientific Singapore 2006
International Journal of
AerospaceEngineeringHindawi Publishing Corporationhttpwwwhindawicom Volume 2014
RoboticsJournal of
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
Active and Passive Electronic Components
Control Scienceand Engineering
Journal of
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
International Journal of
RotatingMachinery
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
Hindawi Publishing Corporation httpwwwhindawicom
Journal ofEngineeringVolume 2014
Submit your manuscripts athttpwwwhindawicom
VLSI Design
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
Shock and Vibration
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
Civil EngineeringAdvances in
Acoustics and VibrationAdvances in
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
Electrical and Computer Engineering
Journal of
Advances inOptoElectronics
Hindawi Publishing Corporation httpwwwhindawicom
Volume 2014
The Scientific World JournalHindawi Publishing Corporation httpwwwhindawicom Volume 2014
SensorsJournal of
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
Modelling amp Simulation in EngineeringHindawi Publishing Corporation httpwwwhindawicom Volume 2014
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
Chemical EngineeringInternational Journal of Antennas and
Propagation
International Journal of
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
Navigation and Observation
International Journal of
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
DistributedSensor Networks
International Journal of
Advances in Acoustics and Vibration 5
times cos119906radic1199102minus 1
119910cos
119906radic11991021205812minus 1
119910
+ 4radic1199102minus 1radic119910
21205812minus 1
times(119906
1205812radic11991021205812minus 1
minus
119906radic11991021205812minus 1
1199102
)
times cos119906radic1199102minus 1
119910cos
119906radic11991021205812minus 1
119910
+ 4119910 (1199102minus 2) sin
119906radic1199102minus 1
119910cos
119906radic11991021205812minus 1
119910
+(4119910radic1199102minus 1 cos
119906radic1199102minus 1
119910
times sin119906radic11991021205812minus 1
119910)(1205812radic11991021205812minus 1)
minus1
+(4119910radic11991021205812minus 1 cos
119906radic1199102minus 1
119910
times sin119906radic11991021205812minus 1
119910)(radic119910
2minus 1)
minus1
minus 4radic1199102minus 1radic119910
21205812minus 1(
119906
radic1199102minus 1
minus
119906radic1199102minus 1
1199102
)
times sin119906radic1199102minus 1
119910sin
119906radic11991021205812minus 1
119910
minus (1199102minus 2)2
(119906
1205812radic11991021205812minus 1
minus
119906radic11991021205812minus 1
1199102
)
times sin119906radic1199102minus 1
119910sin
119906radic11991021205812minus 1
119910
(A1)
B The Mode 1198783119899
for 120581 = 2
For 119910 ≫ 1 radic1199102 minus 1119910 ≃ 1 minus 1(21199102) and radic(11991024) minus 1119910 ≃12 minus 1119910
2
Let 119906119899≃ 2119899120587+(120572
1198991199102) and ignore the terms of order 11199104
or higher Then
cos(radic1199102minus 1
119910119906119899) ≃ 1
cos(radic11991024 minus 1
119910119906119899) ≃ minus1
sin(radic1199102minus 1
119910119906119899) ≃ sin
120572119899minus 119899120587
1199102
≃120572119899minus 119899120587
1199102
sin(radic11991024 minus 1
119910119906119899) ≃ ∓ sin
120572119899minus 2119899120587
1199102
≃ ∓120572119899minus 2119899120587
1199102
(B1)
Putting these expressions in (6) we have
minus1199104120572119899 minus 119899120587
1199102
∓ 2 (120572119899minus 2119899120587) = 0 (B2)
or
(1199102plusmn 2) 120572
119899= 119899120587119910
2∓ 4119899120587 (B3)
or
120572119899=1198991205871199102∓ 4119899120587
1199102plusmn 2
≃ 119899120587 (B4)
for large 119910This result shows that the modes 119878
3119899 119899 = 1 2 3
intersect the line 119910 = 1199100 for large 119910
0 at points slightly to
the right of 119906119899= 2119899120587 119899 = 1 2 3
Acknowledgment
Faiz Ahmad is grateful to the Higher Education Commissionof Pakistan for financial support
References
[1] J D Achenbach Wave Propagation in Elastic Solids chapter 6North-Holland Amsterdam The Netherlands 1980
[2] A H Meitzler ldquoBackward wave tranmission stress pulses inelstic cylinders and platesrdquo Journal of the Acoustical Society ofAmerica vol 38 pp 835ndash842 1965
[3] C Prada D Clorennec and D Royer ldquoLocal vibration of anelastic plate and zero-group velocity Lamb modesrdquo Journal ofthe Acoustical Society of America vol 124 no 1 pp 203ndash2122008
[4] K Nishimiya K Mizutani N Wakatsuki and K YamamotoldquoDetermination of 12 condition for fastest NGV of Lamb-Typewaves under each density ratio of solid and liquid layersrdquoAcoustics 08 Paris pp 3613ndash3618
6 Advances in Acoustics and Vibration
[5] J Wolf T D K Nook R Kille andW G Mayer ldquoInvestigationof lamb waves having negative group velocityrdquo Journal of theAcoustical Society of America vol 83 pp 122ndash126 1988
[6] O Balogun T W Murray and C Prada ldquoSimulation andmeasurement of the optical excitation of the S1 zero groupvelocity Lamb wave resonance in platesrdquo Journal of AppliedPhysics vol 102 no 6 Article ID 064914 2007
[7] K Negishi ldquoNegative group velocities of Lamb wavesrdquo Journalof the Acoustical Society of America vol 64 no 1 p S63 1978
[8] M Germano A Alippi A Bettucci and G Mancuso ldquoAnoma-lous and negative reflection of Lamb waves in mode conver-sionrdquo Physical Review B vol 85 no 1 Article ID 012102 2012
[9] I Tolstoy and E Usdin ldquoWave propagation in elastic plates lowand high mode dispersionrdquo Journal of the Acoustical Society ofAmerica vol 29 pp 37ndash42 1957
[10] M F Werby and H Uberall ldquoThe analysis and interpretation ofsome special properties of higher order symmetric Lambwavesthe case for platesrdquo Journal of the Acoustical Society of Americavol 111 no 6 pp 2686ndash2691 2002
[11] N A Whitaker Jr and H A Haus ldquoBackward wave effectin acoustic scattering measurementsrdquo IEEE Ultrasonics Sympo-sium pp 891ndash894 1983
[12] H Uberall B Hosten M Deschamps and A Gerard ldquoRepul-sion of phase-velocity dispersion curves and the nature of platevibrationsrdquo Journal of the Acoustical Society of America vol 96no 2 pp 908ndash917 1994
[13] T Hussain and F Ahmad ldquoLamb modes with multiple zero-group velocity points in an orthotropic platerdquo Journal of theAcoustical Society of America vol 32 pp 641ndash645 2012
[14] R D Mindlin An Introduction To the Mathematical Theory ofVibrations of Elastic Plates Monograph Sec 211 US ArmySignal Corps Eng Lab Ft Monmouth NJ USA 1995 Editedby J Yang World Scientific Singapore 2006
International Journal of
AerospaceEngineeringHindawi Publishing Corporationhttpwwwhindawicom Volume 2014
RoboticsJournal of
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
Active and Passive Electronic Components
Control Scienceand Engineering
Journal of
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
International Journal of
RotatingMachinery
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
Hindawi Publishing Corporation httpwwwhindawicom
Journal ofEngineeringVolume 2014
Submit your manuscripts athttpwwwhindawicom
VLSI Design
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
Shock and Vibration
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
Civil EngineeringAdvances in
Acoustics and VibrationAdvances in
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
Electrical and Computer Engineering
Journal of
Advances inOptoElectronics
Hindawi Publishing Corporation httpwwwhindawicom
Volume 2014
The Scientific World JournalHindawi Publishing Corporation httpwwwhindawicom Volume 2014
SensorsJournal of
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
Modelling amp Simulation in EngineeringHindawi Publishing Corporation httpwwwhindawicom Volume 2014
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
Chemical EngineeringInternational Journal of Antennas and
Propagation
International Journal of
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
Navigation and Observation
International Journal of
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
DistributedSensor Networks
International Journal of
6 Advances in Acoustics and Vibration
[5] J Wolf T D K Nook R Kille andW G Mayer ldquoInvestigationof lamb waves having negative group velocityrdquo Journal of theAcoustical Society of America vol 83 pp 122ndash126 1988
[6] O Balogun T W Murray and C Prada ldquoSimulation andmeasurement of the optical excitation of the S1 zero groupvelocity Lamb wave resonance in platesrdquo Journal of AppliedPhysics vol 102 no 6 Article ID 064914 2007
[7] K Negishi ldquoNegative group velocities of Lamb wavesrdquo Journalof the Acoustical Society of America vol 64 no 1 p S63 1978
[8] M Germano A Alippi A Bettucci and G Mancuso ldquoAnoma-lous and negative reflection of Lamb waves in mode conver-sionrdquo Physical Review B vol 85 no 1 Article ID 012102 2012
[9] I Tolstoy and E Usdin ldquoWave propagation in elastic plates lowand high mode dispersionrdquo Journal of the Acoustical Society ofAmerica vol 29 pp 37ndash42 1957
[10] M F Werby and H Uberall ldquoThe analysis and interpretation ofsome special properties of higher order symmetric Lambwavesthe case for platesrdquo Journal of the Acoustical Society of Americavol 111 no 6 pp 2686ndash2691 2002
[11] N A Whitaker Jr and H A Haus ldquoBackward wave effectin acoustic scattering measurementsrdquo IEEE Ultrasonics Sympo-sium pp 891ndash894 1983
[12] H Uberall B Hosten M Deschamps and A Gerard ldquoRepul-sion of phase-velocity dispersion curves and the nature of platevibrationsrdquo Journal of the Acoustical Society of America vol 96no 2 pp 908ndash917 1994
[13] T Hussain and F Ahmad ldquoLamb modes with multiple zero-group velocity points in an orthotropic platerdquo Journal of theAcoustical Society of America vol 32 pp 641ndash645 2012
[14] R D Mindlin An Introduction To the Mathematical Theory ofVibrations of Elastic Plates Monograph Sec 211 US ArmySignal Corps Eng Lab Ft Monmouth NJ USA 1995 Editedby J Yang World Scientific Singapore 2006
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Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
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Hindawi Publishing Corporation httpwwwhindawicom
Volume 2014
The Scientific World JournalHindawi Publishing Corporation httpwwwhindawicom Volume 2014
SensorsJournal of
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Modelling amp Simulation in EngineeringHindawi Publishing Corporation httpwwwhindawicom Volume 2014
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Chemical EngineeringInternational Journal of Antennas and
Propagation
International Journal of
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
Navigation and Observation
International Journal of
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
DistributedSensor Networks
International Journal of
International Journal of
AerospaceEngineeringHindawi Publishing Corporationhttpwwwhindawicom Volume 2014
RoboticsJournal of
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
Active and Passive Electronic Components
Control Scienceand Engineering
Journal of
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
International Journal of
RotatingMachinery
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
Hindawi Publishing Corporation httpwwwhindawicom
Journal ofEngineeringVolume 2014
Submit your manuscripts athttpwwwhindawicom
VLSI Design
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
Shock and Vibration
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
Civil EngineeringAdvances in
Acoustics and VibrationAdvances in
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
Electrical and Computer Engineering
Journal of
Advances inOptoElectronics
Hindawi Publishing Corporation httpwwwhindawicom
Volume 2014
The Scientific World JournalHindawi Publishing Corporation httpwwwhindawicom Volume 2014
SensorsJournal of
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
Modelling amp Simulation in EngineeringHindawi Publishing Corporation httpwwwhindawicom Volume 2014
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
Chemical EngineeringInternational Journal of Antennas and
Propagation
International Journal of
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
Navigation and Observation
International Journal of
Hindawi Publishing Corporationhttpwwwhindawicom Volume 2014
DistributedSensor Networks
International Journal of