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OMPARITIVE STUDY OF SKEW DECK SLABS&ITH ORTHOGONAL PARALLELOGRAMESHES OF GRILLAGE ANALOGY
ACHUTHA.oll No 05011D 2002
GUIDED BY.MRS P SRI LAKSHMI
DEPT OF CIVIL ENGINEERING,JNTU HYDERABAD
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YPES OF BRIDGE DECKS
hallow type bridge decks Slab type
Beam and slab type
Voided slab bridge
ellular type bridge decks Single cell bridge
Multiple cell bridge
Multispan bridge with steel boxesMultispan bridge with concrete boxes
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OADING ON BRIDGE:ead Loads ( , ,Permanent stationary loads wearing coat kerb parapets
.,)etc :ive Loads IRC Class A Loading single Lane and Two Lanes
IRC Class 70R Loading
,0R train loading weighing 100 tones through seven axles one,xle of 8 tones two axles of 12 tones each and four axles of
.7 tones each:mpact loading
Value of impact load is a percent of live load depending upon
the material used in the construction of the deck of the
,bridge type of loading and bridge span
, , :oot Way Kerb Railing and Parapet Live Load .For effective span of 7 5 m or less the foot way live load
considered is 400 kg m-2
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TEPS FOLLOWED IN THEETHOD OF GRILLAGE ANALYSISIdealisation of physical deck into equivalent
grillage
Evaluation of equivalent elastic inertia of members
of grillage
Application and transfer of loads to various nodes
of grillage
Determination of force responses and design
envelopes and
Interpretation of results
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DEALIZATION OF PHYSICAL DECK INTOQUIVALENT GRILLAGE.1 Direction of longitudinal grid line is parallel to free edge of
.deck
.2 .Longitudinal grid lines at either edge placed 0 3 D from the edge
, .for slab bridges where D is the depth of the deck
.3 .Longitudinal gird lines are placed along the centre of each bearing
.4 .Minimum of five grid lines are adopted in each direction
.5 .Grid lines are taken at right angles
.6 .Grid lines in general should coincide with the CG of the section
, , .Some shift if it simplifies the idealisation can be made
.7 ,For better results the ratio of the grid spacing in the
.longitudinal and transverse directions should lie between 1 0 to
. .2 0
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b/d 1 1.2 1.5 2 2.5 3 4 5 10 0.141 0.166 0.196 0.229 0.249 0.263 0.281 0.291 0.312 0.333
or rectangular sections = bd >here b d
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UMERICAL ANALYSISNPUT DATAridge data
Deck slab thickness 200 mm
- -Girder to girder spacing .1 875 m
Road width .7 5 m
Effective span 20 m
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Longitudinal Girders1880
800 200
70 150
70
250 1500
760
70
250
300
S.NO AREA B H K KBH3 IZZ Y AY AY2
1 120000 800 150 0.294 7.937E+08 2.250E+08 75 9000000 675000000
2 4900 70 70 0.123 2.961E+06 1.334E+06 173 849333.3333 147217777.8
3 225000 250 900 0.275 3.867E+09 1.519E+10 600 135000000 81000000000
4 1750 25 70 0.258 2.826E+05 4.764E+05 1027 1796666.667 1844577778
5 75000 300 250 0.158 7.422E+08 3.906E+08 1175 88125000 1.03547E+11
426650 IXX= 5.406E+09 1.580E+10 3050 234771000 1.87214E+11
YC=A*Z/A = 550 mm Ig=Iself+A*Y2 = 0.2030m4
Y_TOP = 550 mm IN.A(ZZ) =IG-A*YC2 = 0.0738m4
Y_BOTTOM = 750 mm Ixx = 0.0054m4
I = 0.0738m4
Z_TOP = 0.1342m3
Z_BOTTOM= 0.0985m3
PROPERTIES FOR GRILLAGE ANALYSIS
COMPONENT
800x 150
70x 70
250x 900
25x 70
300x 250
1880
800
70
70
70
1500
150
760
250
200
300
250
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Composite section
S.NO AREA B H K KBH3 IZZ Y AY AY2
1 376000 1880 200 0.311 4.677E+09 1.253E+09 100 37600000 3760000000
2 120000 800 150 0.294 7.937E+08 2.250E+08 275 33000000 9075000000
3 4900 70 70 0.123 2.961E+06 1.334E+06 373 1829333.333 682951111.1
4 225000 250 900 0.275 3.867E+09 1.519E+10 800 180000000 1.44E+11
5 1750 25 70 0.258 2.826E+05 4.764E+05 1227 2146666.667 2633244444
6 75000 300 250 0.158 7.422E+08 3.906E+08 1375 103125000 1.41797E+11
802650 IXX= 1.008E+10 1.706E+10 4150 357701000 3.01948E+11
YC=A*Z/A = 446 mm Ig=Iself+A*Y2 = 0.3190 m4
YTS 446 mm IN.A(ZZ) =IG-A*YC2 = 0.1596 m4 Y_TOP = 246 mm Ixx = 0.0101 m4
Y_BOTTOM 1054 mm
I C = 0.1596 m4
Z_TS= 0.3581 m3
Z_TOP = 0.6497 m3
Z_BOTTOM= 0.1514 m3
Intermediate slab members
1.8800
A = 0.3760 m2 0.200
Iz = 1.8800 x 0.2003 =
0.00125m412
Ix = 2 x 0.00125 = 0.00251 m4
PROPERTIES FOR GRILLAGE ANALYSIS
300x 250
COMPONENT
1880x 200
800x 150
70x 70
250x 900
25x 70
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End slab members0.940
A = 0.1880 m2 0.200
Iz = 0.9400 x 0.200 3 = 0.00063 m4
12
Ix = 2 x 0.00063 = 0.00125 m4
Transverse Members
End Crossgirder 1.000
0.200
A Yt Ayt Ayt2 Iself
0.2000 0.1000 0.0200 0.0020 0.0007 1.050
0.3150 0.7250 0.2284 0.1656 0.0289
0.5150 0.2484 0.1676 0.0296
0.300
Yt = 0.2484 = 0.4823 m
0.5150
Iz = 0.0296 + 0.1676 - 0.2484 x 0.4823 = 0.0774 m4
Ix = 0.276 x 1.000 x 0.200 3
+ 0.294 x 1.050 x 0.300 3
= 0.0105 m4
PROPERTIES FOR GRILLAGE ANALYSIS
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Intermediate Crossgirder 2.0000.200
A Yt Ayt Ayt2 Iself
0.4000 0.1000 0.0400 0.0040 0.0013 1.0500.3150 0.7250 0.2284 0.1656 0.0289
0.7150 0.2684 0.1696 0.0303
0.300
Yt = 0.2684 = 0.3753 m
0.7150
Iz = 0.0303 + 0.1696 - 0.2684 x 0.3753
= 0.0991 m4
Ix = 0.276 x 2.000 x 0.200 3
+ 0.294 x 1.050 x 0.300 3
= 0.0128 m4
Slab members
2.000
A = 0.400 m2 0.200
Iz = 2.000 x 0.200 3 = 0.00133 m4
12
Ix = 2 x 0.00133 = 0.00267 m4
PROPERTIES FOR GRILLAGE ANALYSIS
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LASSIFICATION OF GRILLAGEMODELLING
15 degree skew parallelogram mesh 15 degree skew orthogonal mesh
30 degree skew parallelogram mesh30 degree skew orthogonal mesh
45 degree skew parallelogram mesh 45 degree skew orthogonal mesh
arallelogram mesh rthogonal meshOADING DATA CONSIDERED
RC Class 70 R train loading weighing 000 KN wo lanes of IRC Class A loading each weighing 54 KN
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OUTPUT ( ), ( )Decks are evaluated for bending moment BM shear force SF and
( )torsional moment TM for parallelogram and orthogonal meshes
, ,Variation of BM SF TM for skew angles 00, 50 , 150 , 300, 45 0
studied
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ESULTS ANDDISCUSSION
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DENTIFICATION OF CRITICALGIRDER
. ( ) :Fig 5 0 i Variation of Bending Moment values as a function of span fordifferent Girders for skew angle 00 in parallelogram mesh with IRC Class
70R wheel loading
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DENTIFICATION OF CRITICALGIRDER
. ( ) :Fig 5 1 i Variation of Bending Moment values as a function of span fordifferent Girders for skew angle 50 in parallelogram mesh with IRC Class
70R wheel loading
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DENTIFICATION OF CRITICALGIRDER
. ( ) :Fig 5 2 i Variation of Bending Moment values as a function of span fordifferent Girders for skew angle 150 in parallelogram mesh with IRC Class
70R wheel loading
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DENTIFICATION OF CRITICALGIRDER
. ( ) :Fig 5 3 i Variation of Bending Moment values as a function of span fordifferent Girders for skew angle 300 in parallelogram mesh with IRC Class
70R wheel loading
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DENTIFICATION OF CRITICALGIRDER
. ( ) :Fig 5 4 i Variation of Bending Moment values as a function of span fordifferent Girders for skew angle 450 in parallelogram mesh with IRC Class
70R wheel loading
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DENTIFICATION OF CRITICALGIRDER
. ( ) :Fig 5 0 ii Variation of Shear Force as a function of span for differentGirders for skew angle 00 in parallelogram mesh with IRC Class 70R wheel
loading
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DENTIFICATION OF CRITICALGIRDER
. ( ) :Fig 5 1 ii Variation of Shear Force as a function of span for differentGirders for skew angle 50in parallelogram mesh with IRC Class 70R wheel
loading
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DENTIFICATION OF CRITICALGIRDER
. ( ) :Fig 5 2 ii Variation of Shear Force as a function of span for differentGirders for skew angle 150in parallelogram mesh with IRC Class 70R wheel
loading
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DENTIFICATION OF CRITICALGIRDER
. ( ) :Fig 5 3 ii Variation of Shear Force as a function of span for differentGirders for skew angle 300 in parallelogram mesh with IRC Class 70R wheel
loading
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DENTIFICATION OF CRITICALGIRDER
. ( ) :Fig 5 4 ii Variation of Shear Force as a function of span for differentGirders for skew angle 450 in parallelogram mesh with IRC Class 70R wheel
loading
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DENTIFICATION OF CRITICALGIRDER
. ( ) :Fig 5 0 iii Variation of TorsoinalMoment as a function of span fordifferent Girders for skew angle 00 in parallelogram mesh with IRC Class
70R wheel loading
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DENTIFICATION OF CRITICALGIRDER
. ( ) :Fig 5 1 iii Variation of TorsoinalMoment as a function of span fordifferent Girders for skew angle 50 in parallelogram mesh with IRC Class
70R wheel loading
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DENTIFICATION OF CRITICALGIRDER
. ( ) :Fig 5 2 iii Variation of TorsoinalMoment as a function of span fordifferent Girders for skew angle 150 in parallelogram mesh with IRC Class
70R wheel loading
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DENTIFICATION OF CRITICALGIRDER
. ( ) :Fig 5 3 iii Variation of TorsoinalMoment as a function of span for differentGirders for skew angle 300 in parallelogram mesh with IRC Class 70R wheel
loading
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DENTIFICATION OF CRITICALGIRDER
. ( ) :Fig 5 4 iii Variation of TorsoinalMoment as a function of span fordifferent Girders for skew angle 400 in parallelogram mesh with IRC Class
70R wheel loading
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DENTIFICATION OF LOADS
. . ( ) :Fig 5 5 i Shows Bending Moment values for two lanes of IRC Class A loadingand IRC Class 70R wheel loading for skew angle 00 parallelogram mesh
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DENTIFICATION OF LOADS
. . ( ) :Fig 5 6 i Shows Bending Moment values for two lanes of IRC Class A loadingand IRC Class 70R wheel loading for skew angle 50parallelogram mesh
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DENTIFICATION OF LOADS
. . ( ) :Fig 5 7 i Shows Bending Moment values for two lanes of IRC Class A loadingand IRC Class 70R wheel loading for skew angle 150parallelogram mesh
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DENTIFICATION OF LOADS
. . ( ) :Fig 5 8 i Shows Bending Moment values for two lanes of IRC Class A loadingand IRC Class 70R wheel loading for skew angle 150 parallelogram mesh
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DENTIFICATION OF LOADS
. . ( ) :Fig 5 9 i Shows Bending Moment values for two lanes of IRC Class A loadingand IRC Class 70R wheel loading for skew angle 150parallelogram mesh
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DENTIFICATION OF LOADS
. ( ) :Fig 5 5 ii Shows the variation of Shear Force for IRC Class 70R wheelloading and two lanes of IRC Class A loading for skew angle 00parallelogram
mesh
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DENTIFICATION OF LOADS
. ( ) :Fig 5 6 ii Shows the variation of Shear Force for IRC Class 70R wheelloading and two lanes of IRC Class A loading for skew angle 50parallelogram
mesh
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DENTIFICATION OF LOADS
. ( ) :Fig 5 7 ii Shows the variation of Shear Force for IRC Class 70R wheelloading and two lanes of IRC Class A loading for skew angle 150parallelogram
mesh
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DENTIFICATION OF LOADS
. ( ) :Fig 5 8 ii Shows the variation of Shear Force for IRC Class 70R wheelloading and two lanes of IRC Class A loading for skew angle 300parallelogram
mesh
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DENTIFICATION OF LOADS
. ( ) :Fig 5 9 ii Shows the variation of Shear Force for IRC Class 70R wheelloading and two lanes of IRC Class A loading for skew angle 450parallelogram
mesh
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DENTIFICATION OF LOADS
. . ( ) :Fig 5 5 iii Shows the variation of Shear Force for two lanes of IRC Class Aloading and IRC Class 70R wheel loading for skew angle 00parallelogram mesh
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DENTIFICATION OF LOADS
. . ( ) :Fig 5 6 iii Shows the variation of Shear Force for two lanes of IRC ClassA loading and IRC Class 70R wheel loading for skew angle 50parallelogram
mesh
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DENTIFICATION OF LOADS
. . ( ) :Fig 5 7 iii Shows the variation of Shear Force for two lanes of IRC Class Aloading and IRC Class 70R wheel loading for skew angle 150parallelogram
mesh
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DENTIFICATION OF LOADS
. . ( ) :Fig 5 8 iii Shows the variation of Shear Force for two lanes of IRC Class Aloading and IRC Class 70R wheel loading for skew angle 300parallelogram
mesh
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DENTIFICATION OF LOADS
. . ( ) :Fig 5 9 iii Shows the variation of Shear Force for two lanes of IRC Class Aloading and IRC Class 70R wheel loading for skew angle 450parallelogram
mesh
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UANTITATIVE COMPARISON SHEAR FORCEOR PARALLOGRAM MESH AND ORTHOGONALMESH
. ( ):Fig 5 10 ii Shows the variation of Shear Force for parallogrammesh andorthogonal mesh for skew angle
50
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UANTITATIVE COMPARISON TORSIONALOMENT FOR PARALLOGRAM MESH ANDRTHOGONAL MESH
. ( ):Fig 5 10 ii Shows the Variation of TorsionalMoment for parallogram mesh andorthogonal mesh for skew angle 50
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UANTITATIVE COMPARISON BENDINGOMENT FOR PARALLOGRAM MESH ANDRTHOGONAL MESH
. ( ):Fig 5 10 i Shows variation of the Bending Moment for parallogram mesh andorthogonal mesh for skew angle 50
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UANTITATIVE COMPARISON SHEAR FORCEOR PARALLOGRAM MESH AND ORTHOGONALMESH
. ( ):Fig 5 11 ii Shows the variation of Shear Force for parallogram mesh andorthogonal mesh for skew angle 150
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. ( ):Fig 5 11 iii Shows the variation of TorsionalMoment for parallogram mesh andorthogonal mesh for skew angle 150
UANTITATIVE COMPARISON TORSIONALOMENT FOR PARALLOGRAM MESH ANDRTHOGONAL MESH
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. ( ):Fig 5 11 i Shows the variation of Bending Moment for parallogram mesh andorthogonal mesh for skew angle 150
UANTITATIVE COMPARISON BENDINGOMENT FOR PARALLOGRAM MESH ANDRTHOGONAL MESH
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UANTITATIVE COMPARISON SHEAR FORCEOR PARALLOGRAM MESH AND ORTHOGONALMESH
. ( ):Fig 5 12 ii Shows the variation of Shear Force for parallogram mesh andorthogonal mesh for skew angle 300
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. ( ):Fig 5 12 iii Shows the variation of TorsionalMoment for parallogram mesh andorthogonal mesh for skew angle 300
UANTITATIVE COMPARISON TORSIONALOMENT FOR PARALLOGRAM MESH ANDRTHOGONAL MESH
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. ( ):Fig 5 12 i Shows the variation of Bending Moment for parallogram mesh andorthogonal mesh for skew angle 300
UANTITATIVE COMPARISON BENDINGOMENT FOR PARALLOGRAM MESH ANDRTHOGONAL MESH
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UANTITATIVE COMPARISON SHEAR FORCEOR PARALLOGRAM MESH AND ORTHOGONALMESH
. ( ):Fig 5 13 ii Shows the variation of Shear Force for parallogrammesh andorthogonal mesh for skew angle 450
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. ( ):Fig 5 13 iii Shows the variation of TorsionalMoment for parallogram mesh andorthogonal mesh for skew angle 450
UANTITATIVE COMPARISON TORSIONALOMENT FOR PARALLOGRAM MESH ANDRTHOGONAL MESH
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UANTITATIVE COMPARISON BENDINGOMENT FOR PARALLOGRAM MESH ANDRTHOGONAL MESH
. ( ):Fig 5 13 i Shows the variation of Bending Moment for parallogram mesh andorthogonal mesh for skew angle 450
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, ,UANTITATIVE COMPARISON OF BM TM SFOR PARALLELOGRAM AND ORTHOGONALMESHES
. ( ):Table 5 15 ii Values of Shear Force with respect to skew angels fororthogonal mesh
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. ( ):Table 5 15 iii Values of Torsional Moment with respect to skew angels fororthogonal mesh
, ,UANTITATIVE COMPARISON OF BM TM SFOR PARALLELOGRAM AND ORTHOGONALMESHES
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. ( ):Fig 5 15 i Shows the variation of Bending Moment with respect to skew angles for IRC70R wheel loading
, ,UANTITATIVE COMPARISON OF BM TM SFOR PARALLELOGRAM AND ORTHOGONALMESHES
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UMMARY AND CONCLUSIONS
Girder 1 closest to the kerb is the critical girder
Amongst the two loads considered IRC 70R wheel loading is
chosen for further analysis
, , ( %)Values of BM TM SF are same within 2 to 3 for skew angles
less than 150 .both for parallelogram and orthogonal meshesHence parallogram mesh should be considered for further
.analysis
For skew angles greater than 150 orthogonal mesh should be
, ,chosen for further analysis since the values for BM TM SF are( %) .higher 8 to 30 for parallogrammesh Such choice ensures
.safety and economy