AA-SM-000 Aluminum Material Data

Standard Stress Methods Doc: AA-SM-XX

Revision: A

Material Properties Page: 1

C.1 Derivation of Plastic Buckling Allowables

C.1.1 Approximation of Stress/Strain Curves

Eqn: C.1

Eqn: C.2

Eqn: C.3

Eqn: C.4

Eqn: C.5

In order for material plasticity effects on buckling behaviour to be derived the stress strain curve must be created. For this analysis the Ramberg Osgood method as defined in the Mil-Hdbk-5H equation 9.3.2.4(b) will be used

This expression is valid for tension and compression. For Shear stress strain this expression can be adapted to the material shear behaviour in the following way

The effect of material plasticity of buckling behaviour will be modelled using the following expressions.

For shear and compression buckling the elastic allowable was derived using the method in NACA technical Note 3781, Equation 1, general buckling stress equation:

A modification will be made to the shape factor in the plastic region to more accurately model the stress/strain curve:

This equation can be derived from the figure on Page 9.79 of Mil-Hdbk-5H.This equation can be adapted for shear stress in the same manner as the Ramberg Osgood Stress/Strain Approximation:

Prepared by: R. Abbott Date: Jan 2008 Checked by:___________________Date:__________


Revision: A


C.1.2 Shear Buckling Correction for Material Plasticity effects

Eqn: C.6

Eqn: C.7

C.1.3

Eqn: C.8

Where Gs, the Secant Shear Modulus, is:

Other derivations used for Shear Buckling Data:

Shear Shape Factor (n)

The shear stress/strain curve shape factor can be derived from the known tension and compression shape factor using the following expression:

Where:ns = Shear Shape FactorncL =Compression shape factor in the longitudinal grain directionncLT = Compression shape factor in the longitudinal transverse grain directionntL = Tension shape factor in the longitudinal grain directionntLT = Tension shape factor in the longitudinal transverse grain direction

)

Gs

G

NACA recommends to use a shear plasticity factor based on a plastically corrected poissons ratio of Es/E. Bruhn chapter C5 recommends to use a Gs/G uncorrected for poissons ratio. As the shear stiffness of the material is based on the shear modulus G (even though the allowable stress is related to E - the experimentally determined ks factor accounts for this), and the poissons ratio correction is used in the elastic allowable calculation, it was decided to use a plasticity correction factor as follows:



Revision: A


Shear Yield Stress

the shear yield stress was estimated using equation 9.3.2.6(c) from Ref 1.1

Eqn: C.9

C.1.4 Compression Panel Buckling Correction for Material Plasticity effects

Eqn: C.10

Eqn: C.11

Eqn: C.12

Where Et, the tangent modulus, is

Where Es, the Secant Modulus, is:

Where ve, the plastic poissions ratio, is: (Ref NACA TN 3781 Equation A1)

There is some difficulty selecting a compression allowable plasticity correction factor. Most Aircraft webs and skins do not experience pure compression. Different panels usually experience either pure bending or a combination of bending and compression or bending and tension. Choosing a single plastic correction factor is not possible.After consideration it was decided to use NACA TN 3781 Equation A3 as it fitted closest the physical situation for most of the spar and would be slightly conservative for situations that deviate from pure compression. (Bruhn Fig C5.8)

ν=ν pl−(ν pl−νe )( EsE )

Eqn: C.13



Revision: A


C.1.5 Compression Flange Buckling Correction for Material Plasticity effects

Eqn: C.14

C.1.6 Column Buckling Correction Factor for Material Plasticity effects

Eqn: C.15

The plasticity correction factor for a compression flange will be taken from Bruhn Fig C5.7,

This plasticity correction factor depends on the Secant Modulus, this is defined by Eqn: C.12

This plasticity correction factor uses the poissons ratio correction factor in the plastic region, this is defined by Eqn: C.13

Bruhn section C2.4 gives a method for producing a correction for material plastcity effects based on the tangent modulus. Therefore the following plasticity correction factor will be used:

Et

E

In addition, the plastically corrected inter-rivet buckling allowable curve can be produced. For a rectangular section (Which is implicitly assumed in the inter rivet buckling method) a contant relationship between L/Rho and s/t exists of the square root of 12 (3.464).However where the fixity coefficient C does not equal 4 a correction factor of (4^½)/(C^½) must be applied.

ν=ν pl−(ν pl−νe )( EsE )



Revision: A


C.2 Material Properties for Extruded 7075-T6511 (QQ-A-250/11) - .750/1.499in(Area <20in^2)

LOCATION TITLE

Mil-Hndbk-5F, change notice 2, Table 3.7.6.0 (g1):All Strength Data is A-basis

Ftu L 81000 psiLT 75000 psi Plastic Bending AllowablesST Ref Bruhn C3.4 - Cozzone method

Fty L 72000 psiLT 65000 psiST Rectangular Section

Fcy L 72000 psi k = 1.5LT 71000 psi fbm = 120993 psiST

Fsu 43000 psi Circular SectionFbru 1.5ED 113000 psi k = 1.7

2ED 144000 psi fbm = 136990 psiFbry 1.5ED 93000 psi

2ED 110000 psiElongation 0.07

E - Tension Primary 10400000 psiSecondary 10400000 psi

E-Comp Primary 10700000 psiSecondary 10700000 psi

G 4000000 psiNu 0.33

C.2.1 Plastic Buckling Data for Extruded 7075-T6511 (QQ-A-250/11) - .750/1.499in

Shear BucklingG = 4000000 psi

Fsy = 38590 psiFsu = 43000 psi

31.3

0.07

Compression BucklingEc = 10700000 psi (Minimum of available Ec Values)

Fcy = 71000 psi (Minimum of available Fcy Values)Fcu = 75000 psi (Minimum of available Fcu Values)

26 Shape factor is the Minimum of L and LT values

0.07

ns =

epu =

nc =

epu =

B13

Abbott Aerospace: Do not delete this cell



Revision: A


Derivation of shear Shape Factor, Ref Eqn: C.8

26

27

50

22

( 26 + 27 + 50 + 22 ) / 4

31.3Shape factor taken from nearest billet size/plate thickness

Derivation of Shear Yield Stress, Ref Eqn: C.9

72000 psi

65000 psi

72000 psi

71000 psi

43000 psi

81000 psi

75000 psi

72000 + 65000 + 72000 + 2 x 430004 81000 + 75000

38589.7 Psi

ncL =

ncLT =

ntL =

ntLT =

ns =

ns =

Fty(L) =

Fty(LT) =

Fcy(L) =

Fcy(LT) =

Fsu =

Ftu (L) =

Ftu(LT) =

Fsy =

Fsy =

B74

R Abbott: Do not Delete



Revision: A


C.2.2 Material Properties for Extruded 7075-T6511 (QQ-A-250/11) - .750/1.499in (Continued)Plastic Correction for Shear BucklingLOCATION TITLE

Plastic RambergShear Osgood Secant Gs/G Elastic

Stress Strain Modulus StressEqn: C.5 Eqn: C.3 Eqn: C.7

(Psi) (Psi) (Psi)0 31.25 0.0000 4000000 1.00 0

27013 31.25 0.0068 3999970 1.00 2701327656 31.25 0.0069 3999940 1.00 2765628299 31.25 0.0071 3999879 1.00 2830028942 31.25 0.0072 3999762 1.00 2894429585 31.25 0.0074 3999537 1.00 2958930229 31.25 0.0076 3999112 1.00 3023530872 31.25 0.0077 3998321 1.00 3088531515 31.25 0.0079 3996869 1.00 3154032158 31.25 0.0081 3994234 1.00 3220532801 31.25 0.0082 3989516 1.00 3288733444 31.25 0.0084 3981176 1.00 3360334088 31.25 0.0086 3966630 0.99 3437434731 31.25 0.0088 3941632 0.99 3524535374 31.25 0.0091 3899409 0.97 3628636017 31.25 0.0094 3829615 0.96 3762036660 31.25 0.0099 3717478 0.93 3944637303 31.25 0.0105 3544172 0.89 4210137947 26.98 0.0117 3247416 0.81 4674138590 22.71 0.0131 2944111 0.74 5243039141 22.71 0.0146 2688158 0.67 5824239692 22.71 0.0165 2407930 0.60 6593640244 22.71 0.0190 2114106 0.53 7614340795 22.71 0.0224 1819296 0.45 8969441346 22.71 0.0269 1535947 0.38 10767641897 22.71 0.0329 1274358 0.32 13150942449 22.71 0.0408 1041436 0.26 16303943000 22.71 0.0512 840426 0.21 204658

ns

B129

R Abbott: Fsy x 0.7

B147

R Abbott: Fsy

B155

R Abbott: Fsu



Revision: A


C.2.2 Material Properties for Extruded 7075-T6511 (QQ-A-250/11) - .750/1.499in (Continued)Plastic Correction for Shear Buckling (continued)LOCATION TITLE

Figure: C.2.1 Plastic Correction for Shear Buckling - Extruded 7075-T6511 (QQ-A-250/11) - .750/1.499in

0 20000 40000 60000 80000 100000 120000 140000 160000 180000 2000000

5000

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30000

35000

40000

45000

50000

f(x) = NaN ln(x) NaN

Elastic Shear Stress (psi)

Pla

stic S

hear

Str

ess (

psi)



Revision: A


C.2.3 Material Properties for Extruded 7075-T6511 (QQ-A-250/11) - .750/1.499in (Continued)Plastic Correction for Compressive Plate BucklingLOCATION TITLE

Plastic ElasticCompression Ramberg Tangent Secant v Plasticity Compression

Elastic nc Osgood Modulus Modulus plastic Factor BucklingStress Strain NACA 3781 Stress

Eqn: C.4 Eqn: C.2 Eqn: C.11 Eqn: C.12 Eqn: C.13 Eqn: C.10

(Psi) (Psi) (Psi) (Psi)0 26.00 0.0000 10700000 10700000 0.33 1.00 0

49700 26.00 0.0046 10683960 10699568 0.33 1.00 4971551031 26.00 0.0048 10678269 10699163 0.33 1.00 5105352363 26.00 0.0049 10658706 10698406 0.33 1.00 5240653694 26.00 0.0050 10622908 10697014 0.33 1.00 5377755025 26.00 0.0051 10558655 10694494 0.33 1.00 5518156356 26.00 0.0053 10445807 10689995 0.33 0.99 5664657688 26.00 0.0054 10252747 10682078 0.33 0.99 5821459019 26.00 0.0055 9933483 10668338 0.33 0.98 5995660350 26.00 0.0057 9429201 10644822 0.33 0.97 6198061681 26.00 0.0058 8681254 10605149 0.33 0.96 6443563013 26.00 0.0060 7661538 10539242 0.33 0.93 6750664344 26.00 0.0062 6411598 10431646 0.33 0.90 7138665675 28.43 0.0064 5324051 10332994 0.34 0.87 7532867006 30.86 0.0066 4035931 10156543 0.34 0.83 8060168338 35.72 0.0069 2774922 9907770 0.34 0.78 8711469669 45.43 0.0074 1549434 9469161 0.35 0.72 9630671000 55.15 0.0086 607155 8221861 0.37 0.62 11534771250 60.01 0.0091 460082 7805194 0.38 0.58 12203871500 64.87 0.0098 338515 7269740 0.38 0.54 13123071750 64.87 0.0107 272593 6730867 0.39 0.51 14151572000 64.87 0.0117 219404 6162231 0.40 0.47 15414572250 64.87 0.0130 176552 5576226 0.41 0.43 16970572500 64.87 0.0145 142063 4986767 0.42 0.38 18891772750 64.87 0.0165 114324 4408005 0.43 0.34 21267875000 64.87 0.0770 16491 973908 0.48 0.08 935658

A239

R Abbott: 0.7 * Fcy

A255

R Abbott: Fcy

A263

R Abbott: Fcu = Ftu



Revision: A


C.2.3 Material Properties for Extruded 7075-T6511 (QQ-A-250/11) - .750/1.499in (Continued)Plastic Correction for Compressive Plate Buckling (continued)LOCATION TITLE

Figure: C.2.2 Plastic Correction for Compressive Plate Buckling - Extruded 7075-T6511 (QQ-A-250/11) - .750/1.499in

0 50000 100000 150000 200000 2500000

10000

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30000

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50000

60000

70000

80000

90000f(x) = NaN ln(x) NaN

Elastic Compression Stress (psi)

Pla

sti

c C

om

pre

ss

ion

Str

es

s (

ps

i)



Revision: A


C.2.4 Material Properties for Extruded 7075-T6511 (QQ-A-250/11) - .750/1.499in (Continued)Plastic Correction for Compressive Flange BucklingLOCATION TITLE

Compression Ramberg Secant v Plasticity CompressionPlastic ns Osgood Modulus plastic Factor BucklingStress Strain Stress

Eqn: C.4 Eqn: C.2 Eqn: C.12 Eqn: C.13 Eqn: C.14

(Psi) (Psi) (Psi)0 26.00 0.0000 10700000 0.33 1.00 0

49700 26.00 0.0046 10699568 0.33 1.00 4970251031 26.00 0.0048 10699163 0.33 1.00 5103552363 26.00 0.0049 10698406 0.33 1.00 5236953694 26.00 0.0050 10697014 0.33 1.00 5370755025 26.00 0.0051 10694494 0.33 1.00 5505056356 26.00 0.0053 10689995 0.33 1.00 5640257688 26.00 0.0054 10682078 0.33 1.00 5777259019 26.00 0.0055 10668338 0.33 1.00 5917260350 26.00 0.0057 10644822 0.33 1.00 6062361681 26.00 0.0058 10605149 0.33 0.99 6216363013 26.00 0.0060 10539242 0.33 0.99 6385264344 26.00 0.0062 10431646 0.33 0.98 6578965675 26.00 0.0064 10259618 0.34 0.96 6813567006 26.00 0.0067 9991697 0.34 0.94 7114868338 26.00 0.0071 9588465 0.35 0.91 7523569669 26.00 0.0077 9008409 0.36 0.86 8103771000 64.87 0.0086 8221861 0.37 0.79 8954571250 64.87 0.0092 7768991 0.38 0.75 9450771500 64.87 0.0098 7269740 0.38 0.71 10063971750 64.87 0.0107 6730867 0.39 0.66 10822472000 64.87 0.0117 6162231 0.40 0.61 11761572250 64.87 0.0130 5576226 0.41 0.56 12924872500 64.87 0.0145 4986767 0.42 0.50 14366572750 64.87 0.0165 4408005 0.43 0.45 16153875000 64.87 0.0770 973908 0.48 0.11 707612

A348

R Abbott: Fcy * 0.7

A364

R Abbott: Fcy

A372

R Abbott: Fcu = Fcu



Revision: A


C.2.4 Material Properties for Extruded 7075-T6511 (QQ-A-250/11) - .750/1.499in (Continued)Plastic Correction for Compressive Flange Buckling (continued)LOCATION TITLE

Figure: C.2.3 Plastic Correction for Compressive Flange Buckling - Extruded 7075-T6511 (QQ-A-250/11) - .750/1.499in

0 50000 100000 150000 200000 2500000

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50000

60000

70000

80000

90000

Elastic Flange Compression Stress (psi)

Pla

stic F

lan

ge

Co

mp

ressio

n S

tre

ss (

psi)



Revision: A


C.2.5 Material Properties for Extruded 7075-T6511 (QQ-A-250/11) - .750/1.499in (Continued)Plastic Correction for Column and Inter-Rivet BucklingLOCATION TITLE

ElasticL/Rho Recalculated s/t Fc/Et Compression Tangent Elastic Elastic

L/Rho (Inter-rivet (Strain) Elastic Modulus Johnson Euler buckling) Stress Euler Allowable

Fcs(Psi) (Psi) (Psi) (Psi)

0 0.00 0.0 0.0000 75000 335990 710004 0.74 0.2 18.0809 75000 335990 70793 60750008 1.48 0.4 4.5202 75000 335990 70170 1518750

13 2.22 0.6 2.0090 75000 335990 69133 67500017 2.96 0.9 1.1301 75000 335990 67681 37968821 3.69 1.1 0.7232 75000 335990 65814 24300025 4.43 1.3 0.5022 75000 335990 63532 16875029 5.17 1.5 0.3690 75000 335990 60835 12398033 5.91 1.7 0.2825 75000 335990 57723 9492238 6.65 1.9 0.2232 75000 335990 54197 7500038 10.56 3.0 0.0884 72244 816928 53556 7224439 16.13 4.7 0.0379 69637 1836254 52903 6963740 23.05 6.7 0.0186 67169 3617043 52238 6716940 30.02 8.7 0.0109 64829 5920753 51561 6482941 35.51 10.2 0.0078 62610 7997520 50872 6261042 39.07 11.3 0.0065 60503 9356551 50170 6050342 41.23 11.9 0.0058 58500 10076321 49457 5850043 42.62 12.3 0.0054 56596 10418128 48732 5659644 43.64 12.6 0.0052 54782 10573257 47995 5478245 44.50 12.8 0.0050 53055 10642735 47246 5305545 45.27 13.1 0.0048 51408 10673893 46485 5140846 46.01 13.3 0.0047 49836 10687970 45712 4983647 46.73 13.5 0.0045 48336 10694395 44927 48336

A466

R Abbott: L/Rho equivqlnt to Fcu

47 47.45 13.7 0.0044 46902 10697359 44130 4690248 48.16 13.9 0.0043 45531 10698742 43321 4553149 48.87 14.1 0.0041 44220 10699394 42500 4422050 49.58 14.3 0.0040 42964 10699705 41667 4296450 50.29 14.5 0.0039 41761 10699855 40822 4176151 51.00 14.7 0.0038 40608 10699928 39965 4060852 51.71 14.9 0.0037 39501 10699964 39096 3950152 52.41 15.1 0.0036 38440 10699982 38215 3844053 53.12 15.3 0.0035 37421 10699991 37322 3742154 53.83 15.5 0.0034 36441 10699995 36417 3644155 54.54 15.7 0.0033 35500 10699998 35500 3550065 64.54 18.6 0.0024 25352 10700000 21289 2535275 74.54 21.5 0.0018 19006 10700000 4691 1900685 84.54 24.4 0.0014 14776 10700000 -14293 1477695 94.54 27.3 0.0011 11815 10700000 -35664 11815

105 104.54 30.2 0.0009 9663 10700000 -59422 9663



Revision: A


C.2.5 Material Properties for Extruded 7075-T6511 (QQ-A-250/11) - .750/1.499in (Continued)Plastic Correction for Column and Inter-Rivet Buckling (continued)LOCATION TITLE

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40000

50000

60000

70000

80000

Elastic Euler Column Allow-ableTangent Modulus Based Column Al-lowable

Johnson Column Allowable based on Fcy

L/Rho

Col

umn

failu

re S

tres

s (P

si)

A490

R Abbott: Fcy *.5

Figure: C.2.4



Revision: A


C.2.5 Material Properties for Extruded 7075-T6511 (QQ-A-250/11) - .750/1.499in (Continued)Plastic Correction for Column and Inter-Rivet Buckling (continued)LOCATION TITLE

Plastic Correction for Column Buckling - Extruded 7075-T6511 (QQ-A-250/11) - .750/1.499in

Note that the higher column allowables are likely to be limited by section crippling, therefore the above graph is only applicable for columns with stable cross sections.

0 20 40 60 80 100 1200

10000

20000

30000

40000

50000

60000

70000

80000

Elastic Euler Column Allow-ableTangent Modulus Based Column Al-lowable

Johnson Column Allowable based on Fcy

L/RhoC

olum

n fa

ilure

Str

ess

(Psi

)

0 5 10 15 20 25 30 35 400

10000

20000

30000

40000

50000

60000

70000

80000

s/t

Inte

r-R

ivet

Bucklin

g S

tress (

Psi)

Figure: C.2.5

s = fastener pitcht = sheet thickness


Plastic Correction for Inter-Rivet Buckling - Extruded 7075-T6511 (QQ-A-250/11) - .750/1.499in

0 5 10 15 20 25 30 35 400

10000

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30000

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50000

60000

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80000

s/tIn

ter-

Riv

et

Bucklin

g S

tress (

Psi)

0 1 2 3 4 5 6 7 8

Material Table (MIL-HDBK-5F, notice 2)

Material Material MIL-HDBK Ftu

Code Series Temp Reference Thickness L LT ST

B2014 T6 AMS 4029 3.2.1.0(b1) 0.020/0.039 65 64B2014 T6 AMS 4029 3.2.1.0(b1) 0.040/0.249 67 66B2014 T651 AMS4029 3.2.1.0(b1) 0.250/0.499 66 67B2014 T651 AMS4029 3.2.1.0(b1) 0.500/1.000 66 67B2014 T651 AMS4029 3.2.1.0(b1) 1.001/2.000 66 67B2014 T651 AMS4029 3.2.1.0(b1) 2.001/2.500 64 65 59B2014 T651 AMS4029 3.2.1.0(b1) 2.501/3.000 63B2014 T651 AMS4029 3.2.1.0(b1) 3.001/4.000 59B2024 T3 QQ-A-250/4 3.2.3.0(b1) 0.008/0.009 64 63B2024 T3 QQ-A-250/4 3.2.3.0(b1) 0.010/0.128 64 63B2024 T3 QQ-A-250/4 3.2.3.0(b1) 0.129/0.249 65 64B2024 T351 QQ-A-250/4 3.2.3.0(b1) 0.250/0.499 64 64B2024 T351 QQ-A-250/4 3.2.3.0(b1) .500/1.000 63 63B2024 T351 QQ-A-250/4 3.2.3.0(b1) 1.001/1.500 62 62B2024 T351 QQ-A-250/4 3.2.3.0(b1) 1.501/2.000 62 62B2024 T351 QQ-A-250/4 3.2.3.0(b1) 2.001/3.000 60 60 52B2024 T351 QQ-A-250/4 3.2.3.0(b1) 3.001/4.000 57 57 49

Area <20in^2 E2024 T3 QQ-A-250/3 3.2.3.0 (j1) 0.000/0.249 57 54Area <20in^2 E2024 T3 QQ-A-250/3 3.2.3.0 (j1) 0.250/.499 60 56Area <20in^2 E2024 T3 QQ-A-250/3 3.2.3.0 (j1) .500/.749 60 54Area <20in^2 E2024 T3 QQ-A-250/3 3.2.3.0 (j1) .750/1.499 65 56Area <25in^2 E2024 T3 QQ-A-250/3 3.2.3.0 (j1) 1.500/2.999 70 55Area <25in^2 E2024 T3 QQ-A-250/3 3.2.3.0 (j1) 3.000/4.499 70 54Area >25<32in^2 E2024 T3 QQ-A-250/3 3.2.3.0 (j1) 1.500/2.999 64 64Area >25<32in^2 E2024 T3 QQ-A-250/3 3.2.3.0 (j1) 3.000/4.499 66 64Area <20in^2 E2024 T3510 QQ-A-250/3 3.2.3.0 (j1) 0.000/0.249 57 54Area <20in^2 E2024 T3510 QQ-A-250/3 3.2.3.0 (j1) 0.250/.499 60 56Area <20in^2 E2024 T3510 QQ-A-250/3 3.2.3.0 (j1) .500/.749 60 54Area <20in^2 E2024 T3510 QQ-A-250/3 3.2.3.0 (j1) .750/1.499 65 56Area <25in^2 E2024 T3510 QQ-A-250/3 3.2.3.0 (j1) 1.500/2.999 70 55Area <25in^2 E2024 T3510 QQ-A-250/3 3.2.3.0 (j1) 3.000/4.499 70 54Area >25<32in^2 E2024 T3510 QQ-A-250/3 3.2.3.0 (j1) 1.500/2.999 64 64Area >25<32in^2 E2024 T3510 QQ-A-250/3 3.2.3.0 (j1) 3.000/4.499 66 64Area <20in^2 E2024 T3511 QQ-A-250/3 3.2.3.0 (j1) 0.000/0.249 57 54Area <20in^2 E2024 T3511 QQ-A-250/3 3.2.3.0 (j1) 0.250/.499 60 56Area <20in^2 E2024 T3511 QQ-A-250/3 3.2.3.0 (j1) .500/.749 60 54Area <20in^2 E2024 T3511 QQ-A-250/3 3.2.3.0 (j1) .750/1.499 65 56Area <25in^2 E2024 T3511 QQ-A-250/3 3.2.3.0 (j1) 1.500/2.999 70 55Area <25in^2 E2024 T3511 QQ-A-250/3 3.2.3.0 (j1) 3.000/4.499 70 54

0 1 2 3 4 5 6 7 8



Code Series Temp Reference Thickness L LT STArea >25<32in^2 E2024 T3511 QQ-A-250/3 3.2.3.0 (j1) 1.500/2.999 64 64Area >25<32in^2 E2024 T3511 QQ-A-250/3 3.2.3.0 (j1) 3.000/4.499 66 64

B2024 T4 B2024 T42 QQ-A-250/4 3.2.3.0(b2) 0.010/0.249 62 62B2024 T42 QQ-A-250/4 3.2.3.0(b2) 0.250/0.499 61 62B2024 T42 QQ-A-250/4 3.2.3.0(b2) 0.500/1.000 60 61B2024 T42 QQ-A-250/4 3.2.3.0(b2) 1.001/2.000 59 60B2024 T42 QQ-A-250/4 3.2.3.0(b2) 2.001/3.000 58

Area <25in^2 E2024 T42 QQ-A-200/3 3.2.3.0 (j2) 000/.249 57 55Area <25in^2 E2024 T42 QQ-A-200/3 3.2.3.0 (j2) 0.250/.499 57 54Area <25in^2 E2024 T42 QQ-A-200/3 3.2.3.0 (j2) .500/.749 57 52Area <25in^2 E2024 T42 QQ-A-200/3 3.2.3.0 (j2) .75/.999 57 51Area <25in^2 E2024 T42 QQ-A-200/3 3.2.3.0 (j2) 1.000/1.249 57 49Area <25in^2 E2024 T42 QQ-A-200/3 3.2.3.0 (j2) 1.250/1.499 57 47Area <25in^2 E2024 T42 QQ-A-200/3 3.2.3.0 (j2) 1.500/1.749 57 45Area <25in^2 E2024 T42 QQ-A-200/3 3.2.3.0 (j2) 1.750/1.999 57 43Area <25in^2 E2024 T42 QQ-A-200/3 3.2.3.0 (j2) 2.000/2.249 57 41Area <25in^2 E2024 T42 QQ-A-200/3 3.2.3.0 (j2) 2.250/2.499 57 39

B2024 T6 B6061 T4 QQ-A-250/11 3.6.2.0(b1) 0.010/0.249 30B6061 T6 QQ-A-250/11 3.6.2.0(b1) 0.010/0.249 42 42B6061 T62 QQ-A-250/11 3.6.2.0(b1) 0.010/0.249 42 42B6061 T62 QQ-A-250/11 3.6.2.0(b1) 0.250/2.000 42 42B7075 T6 QQ-A-250/12 3.7.4.0(b1) 0.008/0.011 74B7075 T6 QQ-A-250/12 3.7.4.0(b1) 0.012/0.039 76 76B7075 T6 QQ-A-250/12 3.7.4.0(b1) 0.040/0.125 78 78B7075 T6 QQ-A-250/12 3.7.4.0(b1) 0.126/0.249 78 78B7075 T62 QQ-A-250/12 3.7.4.0(b1) 0.008/0.011 74B7075 T62 QQ-A-250/12 3.7.4.0(b1) 0.012/0.039 76 76B7075 T62 QQ-A-250/12 3.7.4.0(b1) 0.040/0.125 78 78B7075 T62 QQ-A-250/12 3.7.4.0(b1) 0.126/0.249 78 78B7075 T651 QQ-A-250/12 3.7.4.0(b1) 0.250/0.499 77 78B7075 T651 QQ-A-250/12 3.7.4.0(b1) 0.500/1.000 77 78B7075 T651 QQ-A-250/12 3.7.4.0(b1) 1.001/2.000 76 77B7075 T651 QQ-A-250/12 3.7.4.0(b1) 2.001/2.500 75 76 70B7075 T651 QQ-A-250/12 3.7.4.0(b1) 2.501/3.000 71 72 66B7075 T651 QQ-A-250/12 3.7.4.0(b1) 3.001/3.500 70 71 65B7075 T651 QQ-A-250/12 3.7.4.0(b1) 3.501/4.000 66 67 61

Area <20in^2 E7075 T6 QQ-A-250/11 3.7.6.0 (g1) 0.000/0.249 78 75Area <20in^2 E7075 T6 QQ-A-250/11 3.7.6.0 (g1) .249/.499 81 78

0 1 2 3 4 5 6 7 8



Code Series Temp Reference Thickness L LT STArea <20in^2 E7075 T6 QQ-A-250/11 3.7.6.0 (g1) .500/.749 81 77Area <20in^2 E7075 T6 QQ-A-250/11 3.7.6.0 (g1) .750/1.499 81 75Area <20in^2 E7075 T6 QQ-A-250/11 3.7.6.0 (g1) 1.500/2.999 81 71 67Area <20in^2 E7075 T6 QQ-A-250/11 3.7.6.0 (g1) 3.000/4.499 81 67 67Area >20<32in^2 E7075 T6 QQ-A-250/11 3.7.6.0 (g1) 3.000/4.499 78 64 64Area <32in^2 E7075 T6 QQ-A-250/11 3.7.6.0 (g1) 4.500/5.000 78 63 63Area <20in^2 E7075 T6510 QQ-A-250/11 3.7.6.0 (g1) 0.000/0.249 78 75Area <20in^2 E7075 T6510 QQ-A-250/11 3.7.6.0 (g1) .249/.499 81 78Area <20in^2 E7075 T6510 QQ-A-250/11 3.7.6.0 (g1) .500/.749 81 77Area <20in^2 E7075 T6510 QQ-A-250/11 3.7.6.0 (g1) .750/1.499 81 75Area <20in^2 E7075 T6510 QQ-A-250/11 3.7.6.0 (g1) 1.500/2.999 81 71 67Area <20in^2 E7075 T6510 QQ-A-250/11 3.7.6.0 (g1) 3.000/4.499 81 67 67Area >20<32in^2 E7075 T6510 QQ-A-250/11 3.7.6.0 (g1) 3.000/4.499 78 64 64Area <32in^2 E7075 T6510 QQ-A-250/11 3.7.6.0 (g1) 4.500/5.000 78 63 63Area <20in^2 E7075 T6511 QQ-A-250/11 3.7.6.0 (g1) 0.000/0.249 78 75Area <20in^2 E7075 T6511 QQ-A-250/11 3.7.6.0 (g1) .249/.499 81 78Area <20in^2 E7075 T6511 QQ-A-250/11 3.7.6.0 (g1) .500/.749 81 77Area <20in^2 E7075 T6511 QQ-A-250/11 3.7.6.0 (g1) .750/1.499 81 75Area <20in^2 E7075 T6511 QQ-A-250/11 3.7.6.0 (g1) 1.500/2.999 81 71 67Area <20in^2 E7075 T6511 QQ-A-250/11 3.7.6.0 (g1) 3.000/4.499 81 67 67Area >20<32in^2 E7075 T6511 QQ-A-250/11 3.7.6.0 (g1) 3.000/4.499 78 64 64Area <32in^2 E7075 T6511 QQ-A-250/11 3.7.6.0 (g1) 4.500/5.000 78 63 63Area <20in^2 E7075 T62 QQ-A-250/11 3.7.6.0 (g1) 0.000/0.249 78 75Area <20in^2 E7075 T62 QQ-A-250/11 3.7.6.0 (g1) .249/.499 81 78Area <20in^2 E7075 T62 QQ-A-250/11 3.7.6.0 (g1) .500/.749 81 77Area <20in^2 E7075 T62 QQ-A-250/11 3.7.6.0 (g1) .750/1.499 81 75Area <20in^2 E7075 T62 QQ-A-250/11 3.7.6.0 (g1) 1.500/2.999 81 71 67Area <20in^2 E7075 T62 QQ-A-250/11 3.7.6.0 (g1) 3.000/4.499 81 67 67Area >20<32in^2 E7075 T62 QQ-A-250/11 3.7.6.0 (g1) 3.000/4.499 78 64 64Area <32in^2 E7075 T62 QQ-A-250/11 3.7.6.0 (g1) 4.500/5.000 78 63 63

B7075 T73 QQ-A-250/12 3.7.4.0(b3) 0.040/0.249 67 67B7075 T7351 QQ-A-250/12 3.7.4.0(b3) 0.250/0.499 68 69B7075 T7351 QQ-A-250/12 3.7.4.0(b3) 0.500/1.000 68 69B7075 T7351 QQ-A-250/12 3.7.4.0(b3) 1.001/1.500 67 68B7075 T7351 QQ-A-250/12 3.7.4.0(b3) 1.501/2.000 66 67 63B7075 T7351 QQ-A-250/12 3.7.4.0(b3) 2.001/2.500 65 66 62B7075 T7351 QQ-A-250/12 3.7.4.0(b3) 2.501/3.000 63 64 60B7075 T7351 QQ-A-250/12 3.7.4.0(b3) 3.001/3.500 62 63 59B7075 T7351 QQ-A-250/12 3.7.4.0(b3) 3.501/4.000 60 61 57C2014 T6 QQ-A-250/3 3.2.1.0(c1) 0.020/0.039 62 61

0 1 2 3 4 5 6 7 8



Code Series Temp Reference Thickness L LT STC2014 T6 QQ-A-250/3 3.2.1.0(c1) 0.040/0.249 65 64C2014 T651 QQ-A-250/3 3.2.1.0(c1) 0.250/0.499 63 64C2014 T651 QQ-A-250/3 3.2.1.0(c1) 0.500/1.000 63 64C2014 T651 QQ-A-250/3 3.2.1.0(c1) 1.001/2.000 63 64C2014 T651 QQ-A-250/3 3.2.1.0(c1) 2.001/2.500 61 62 59C2014 T651 QQ-A-250/3 3.2.1.0(c1) 2.501/3.000 60C2014 T651 QQ-A-250/3 3.2.1.0(c1) 3.001/4.000 56C2024 T3 QQ-A-250/5 3.2.3.0(e1) 0.008/0.009 59 58C2024 T3 QQ-A-250/5 3.2.3.0(e1) 0.010/0.062 60 59C2024 T3 QQ-A-250/5 3.2.3.0(e1) 0.063/0.128 62 61C2024 T3 QQ-A-250/5 3.2.3.0(e1) 0.129/0.249 63 62C2024 T4 C2024 T42 QQ-A-250/5 3.2.3.0(e3) 0.008/0.009 55 55C2024 T42 QQ-A-250/5 3.2.3.0(e3) 0.010/0.062 57 57C2024 T42 QQ-A-250/5 3.2.3.0(e3) 0.063/0.249 60 60C2024 T42 QQ-A-250/5 3.2.3.0(e3) 0.250/0.499 59 60C2024 T42 QQ-A-250/5 3.2.3.0(e3) 0.500/1.000 58 59C2024 T42 QQ-A-250/5 3.2.3.0(e3) 1.001/2.000 57 58C2024 T42 QQ-A-250/5 3.2.3.0(e3) 2.001/3.000 56C2024 T6 C7075 T6 AMS 4049 3.7.4.0(c1) 0.008/0.011 68C7075 T6 AMS 4049 3.7.4.0(c1) 0.012/0.039 71 71 C7075 T6 AMS 4049 3.7.4.0(c1) 0.040/0.062 71 71 C7075 T6 AMS 4049 3.7.4.0(c1) 0.063/0.187 74 74 C7075 T6 AMS 4049 3.7.4.0(c1) 0.188/0.249 75 75C7075 T62 QQ-A-250/13 3.7.4.0(c2) 0.008/0.011 68C7075 T62 QQ-A-250/13 3.7.4.0(c2) 0.012/0.039 70 70C7075 T62 QQ-A-250/13 3.7.4.0(c2) 0.040/0.062 71 71 C7075 T62 QQ-A-250/13 3.7.4.0(c2) 0.063/0.187 73 73C7075 T62 QQ-A-250/13 3.7.4.0(c2) 0.188/0.249 75 75C7075 T651 QQ-A-250/13 3.7.4.0(c3) 0.250/0.499 74 75C7075 T651 QQ-A-250/13 3.7.4.0(c3) 0.500/1.000 75 76C7075 T651 QQ-A-250/13 3.7.4.0(c3) 1.001/2.000 74 75C7075 T651 QQ-A-250/13 3.7.4.0(c3) 2.001/2.500 73 74 70C7075 T651 QQ-A-250/13 3.7.4.0(c3) 2.501/3.000 69 70 66C7075 T651 QQ-A-250/13 3.7.4.0(c3) 3.001/3.500 68 69 65C7075 T651 QQ-A-250/13 3.7.4.0(c3) 3.501/4.000 64 65 61

9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25

Fty Fcy Fsu Fbru Fbry Elongat. E Ec G

L LT ST L LT ST 1.5ED 2ED 1.5ED 2ED Prim. Sec. Prim. Sec.

58 57 58 59 39 97 123 81 93 6 10.5 10.5 10.7 10.7 459 58 59 60 40 100 127 83 94 7 10.5 10.5 10.7 10.7 460 59 58 61 40 105 134 90 106 7 10.7 10.7 10.9 10.9 460 59 58 61 40 105 134 90 106 6 10.7 10.7 10.9 10.9 460 59 58 61 40 105 134 90 106 4 10.7 10.7 10.9 10.9 459 58 54 57 60 59 38 102 130 88 104 2 10.7 10.7 10.9 10.9 4

57 2 10.7 10.7 10.9 10.9 455 1 10.7 10.7 10.9 10.9 4

47 42 39 45 39 104 129 73 88 10 10.5 10.5 10.7 10.7 447 42 39 45 39 104 129 73 88 10 10.5 10.5 10.7 10.7 447 42 39 45 40 106 131 73 88 10 10.5 10.5 10.7 10.7 448 42 39 45 38 97 119 72 86 12 10.7 10.7 10.9 10.9 448 42 39 45 37 95 117 72 86 8 10.7 10.7 10.9 10.9 447 42 39 44 37 94 115 72 86 7 10.7 10.7 10.9 10.9 447 42 38 44 37 94 115 72 86 6 10.7 10.7 10.9 10.9 446 42 38 37 43 46 35 91 111 72 86 4 10.7 10.7 10.9 10.9 443 41 38 35 41 44 34 86 106 70 84 4 10.7 10.7 10.9 10.9 442 37 34 41 29 84 108 61 71 12 10.8 10.8 11 11 4.144 38 37 41 31 78 98 55 67 12 10.8 10.8 11 11 4.144 37 38 40 30 78 97 55 67 12 10.8 10.8 11 11 4.146 37 41 40 33 84 105 57 69 10 10.8 10.8 11 11 4.152 39 49 42 34 88 111 63 77 10 10.8 10.8 11 11 4.152 39 49 41 33 86 109 62 75 10 10.8 10.8 11 11 4.156 55 57 57 35 94 123 79 93 4 10.8 10.8 11 11 4.158 57 59 59 36 96 123 82 76 5 10.8 10.8 11 11 4.142 37 34 41 29 84 108 61 71 12 10.8 10.8 11 11 4.144 38 37 41 31 78 98 55 67 12 10.8 10.8 11 11 4.144 37 38 40 30 78 97 55 67 12 10.8 10.8 11 11 4.146 37 41 40 33 84 105 57 69 10 10.8 10.8 11 11 4.152 39 49 42 34 88 111 63 77 10 10.8 10.8 11 11 4.152 39 49 41 33 86 109 62 75 10 10.8 10.8 11 11 4.156 55 57 57 35 94 123 79 93 4 10.8 10.8 11 11 4.158 57 59 59 36 96 123 82 76 5 10.8 10.8 11 11 4.142 37 34 41 29 84 108 61 71 12 10.8 10.8 11 11 4.144 38 37 41 31 78 98 55 67 12 10.8 10.8 11 11 4.144 37 38 40 30 78 97 55 67 12 10.8 10.8 11 11 4.146 37 41 40 33 84 105 57 69 10 10.8 10.8 11 11 4.152 39 49 42 34 88 111 63 77 10 10.8 10.8 11 11 4.152 39 49 41 33 86 109 62 75 10 10.8 10.8 11 11 4.1

9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25


L LT ST L LT ST 1.5ED 2ED 1.5ED 2ED Prim. Sec. Prim. Sec.56 55 57 57 35 94 123 79 93 4 10.8 10.8 11 11 4.158 57 59 59 36 96 123 82 76 5 10.8 10.8 11 11 4.1

38 38 38 38 37 93 118 53 61 12 10.5 10.5 10.7 10.7 438 38 40 40 37 88 108 64 75 12 10.7 10.7 10.9 10.9 438 38 40 40 36 86 107 64 75 8 10.7 10.7 10.9 10.9 438 38 40 40 35 85 105 64 75 8 10.7 10.7 10.9 10.9 4

38 4 10.7 10.7 10.9 10.9 438 36 38 39 29 81 99 56 69 12 10.8 10.8 11 11 4.138 35 38 38 29 80 98 55 67 12 10.8 10.8 11 11 4.138 34 38 37 29 79 97 53 65 12 10.8 10.8 11 11 4.138 33 38 36 29 77 95 51 63 10 10.8 10.8 11 11 4.138 32 38 35 29 75 93 49 61 10 10.8 10.8 11 11 4.138 31 38 34 29 74 91 47 59 10 10.8 10.8 11 11 4.138 30 38 33 28 71 89 44 56 10 10.8 10.8 11 11 4.138 29 38 31 27 69 86 41 53 10 10.8 10.8 11 11 4.138 28 38 30 26 67 83 39 50 10 10.8 10.8 11 11 4.128 27 38 29 24 64 81 36 47 10 10.8 10.8 11 11 4.1

16 16 20 48 63 22 26 9.9 9.9 10.1 10.1 3.836 35 35 36 27 67 88 50 58 9.9 9.9 10.1 10.1 3.836 35 35 36 27 67 88 50 58 9.9 9.9 10.1 10.1 3.836 35 35 36 27 67 88 50 58 9.9 9.9 10.1 10.1 3.8

63 5 10.3 10.3 10.5 10.5 3.969 67 68 71 46 118 152 100 117 7 10.3 10.3 10.5 10.5 3.970 68 69 72 47 121 156 102 119 8 10.3 10.3 10.5 10.5 3.971 69 70 73 47 121 156 103 121 8 10.3 10.3 10.5 10.5 3.9

63 5 10.3 10.3 10.5 10.5 3.969 67 68 71 46 118 152 100 117 7 10.3 10.3 10.5 10.5 3.970 68 69 72 47 121 156 102 119 8 10.3 10.3 10.5 10.5 3.971 69 70 73 47 121 156 103 121 8 10.3 10.3 10.5 10.5 3.969 67 67 71 43 117 145 97 114 9 10.3 10.3 10.6 10.6 3.970 68 68 72 44 117 145 100 117 7 10.3 10.3 10.6 10.6 3.969 67 66 71 44 116 143 100 117 6 10.3 10.3 10.6 10.6 3.966 64 59 62 68 67 44 114 141 98 113 5 10.3 10.3 10.6 10.6 3.963 61 56 58 65 64 42 108 134 94 109 5 10.3 10.3 10.6 10.6 3.960 58 54 55 61 61 42 107 132 89 104 5 10.3 10.3 10.6 10.6 3.956 54 50 51 57 57 39 101 124 84 98 3 10.3 10.3 10.6 10.6 3.970 66 70 72 41 111 140 92 108 7 10.4 10.4 10.7 10.7 473 69 73 74 43 115 146 96 113 7 10.4 10.4 10.7 10.7 4

9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25


L LT ST L LT ST 1.5ED 2ED 1.5ED 2ED Prim. Sec. Prim. Sec.72 67 72 73 43 115 145 94 111 7 10.4 10.4 10.7 10.7 472 65 72 71 43 113 144 93 110 7 10.4 10.4 10.7 10.7 472 61 56 72 67 62 42 110 141 89 106 7 10.4 10.4 10.7 10.7 471 56 55 71 62 62 40 106 137 84 101 7 10.4 10.4 10.7 10.7 470 55 55 70 61 61 39 102 132 83 100 6 10.4 10.4 10.7 10.7 468 52 52 68 57 57 38 101 131 79 95 6 10.4 10.4 10.7 10.7 470 66 70 72 41 111 140 92 108 7 10.4 10.4 10.7 10.7 473 69 73 74 43 115 146 96 113 7 10.4 10.4 10.7 10.7 472 67 72 73 43 115 145 94 111 7 10.4 10.4 10.7 10.7 472 65 72 71 43 113 144 93 110 7 10.4 10.4 10.7 10.7 472 61 56 72 67 62 42 110 141 89 106 7 10.4 10.4 10.7 10.7 471 56 55 71 62 62 40 106 137 84 101 7 10.4 10.4 10.7 10.7 470 55 55 70 61 61 39 102 132 83 100 6 10.4 10.4 10.7 10.7 468 52 52 68 57 57 38 101 131 79 95 6 10.4 10.4 10.7 10.7 470 66 70 72 41 111 140 92 108 7 10.4 10.4 10.7 10.7 473 69 73 74 43 115 146 96 113 7 10.4 10.4 10.7 10.7 472 67 72 73 43 115 145 94 111 7 10.4 10.4 10.7 10.7 472 65 72 71 43 113 144 93 110 7 10.4 10.4 10.7 10.7 472 61 56 72 67 62 42 110 141 89 106 7 10.4 10.4 10.7 10.7 471 56 55 71 62 62 40 106 137 84 101 7 10.4 10.4 10.7 10.7 470 55 55 70 61 61 39 102 132 83 100 6 10.4 10.4 10.7 10.7 468 52 52 68 57 57 38 101 131 79 95 6 10.4 10.4 10.7 10.7 470 66 70 72 41 111 140 92 108 7 10.4 10.4 10.7 10.7 473 69 73 74 43 115 146 96 113 7 10.4 10.4 10.7 10.7 472 67 72 73 43 115 145 94 111 7 10.4 10.4 10.7 10.7 472 65 72 71 43 113 144 93 110 7 10.4 10.4 10.7 10.7 472 61 56 72 67 62 42 110 141 89 106 7 10.4 10.4 10.7 10.7 471 56 55 71 62 62 40 106 137 84 101 7 10.4 10.4 10.7 10.7 470 55 55 70 61 61 39 102 132 83 100 6 10.4 10.4 10.7 10.7 468 52 52 68 57 57 38 101 131 79 95 6 10.4 10.4 10.7 10.7 456 56 55 58 38 105 134 84 102 8 10.3 10.3 10.5 10.5 3.957 57 56 59 38 102 131 79 95 7 10.3 10.3 10.6 10.6 3.957 57 56 59 38 103 132 81 97 7 10.3 10.3 10.6 10.6 3.957 57 56 59 38 103 132 83 99 6 10.3 10.3 10.6 10.6 3.955 55 52 53 57 59 39 102 132 82 97 6 10.3 10.3 10.6 10.6 3.952 52 49 50 54 55 39 102 131 79 93 6 10.3 10.3 10.6 10.6 3.949 49 47 47 51 51 38 100 128 76 89 6 10.3 10.3 10.6 10.6 3.949 49 47 47 51 50 38 99 127 76 89 6 10.3 10.3 10.6 10.6 3.948 48 46 45 50 48 37 96 124 96 124 6 10.3 10.3 10.6 10.6 3.954 53 54 55 37 93 117 76 86 7 10.5 10.5 10.7 10.7 4

9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25


L LT ST L LT ST 1.5ED 2ED 1.5ED 2ED Prim. Sec. Prim. Sec.57 56 57 58 39 97 123 80 91 8 10.5 10.5 10.7 10.7 458 57 56 59 38 101 128 87 102 8 10.7 10.7 10.9 10.9 457 56 55 58 38 101 128 85 100 6 10.7 10.7 10.9 10.9 457 56 55 58 38 101 128 85 100 4 10.7 10.7 10.9 10.9 456 55 54 54 57 59 37 97 124 84 98 2 10.7 10.7 10.9 10.9 4

54 2 10.7 10.7 10.9 10.9 452

44 39 36 42 37 96 119 68 82 10 10.5 9.5 10.7 9.7 3.5644 39 36 42 37 97 121 68 82 10.5 9.5 10.7 9.7 3.5645 40 37 43 38 101 125 70 84 15 10.5 10 10.7 10.2 3.7445 40 37 43 39 102 127 70 84 15 10.5 10 10.7 10.2 3.74

34 34 34 34 33 83 104 48 54 10 10.5 9.5 10.7 9.7 3.5634 34 34 34 34 86 108 48 54 10.5 9.5 10.7 9.7 3.5636 36 36 36 36 90 114 50 58 15 10.5 10 10.7 10.2 3.7436 36 37 38 35 85 105 60 71 12 10.7 10.2 10.9 10.4 3.8236 36 37 38 35 83 103 60 71 8 10.7 10.2 10.9 10.4 3.8236 36 37 38 34 82 101 60 71 10.7 10.2 10.9 10.4 3.82

36 4 10.7 10.2 10.9 10.4 3.82

58 5 10.3 9.5 10.5 9.7 3.5662 60 61 64 42 110 142 90 105 8 10.3 9.5 10.5 9.7 3.5663 61 62 65 42 110 142 91 106 9 10.3 9.5 10.5 9.7 3.5666 64 65 68 44 115 148 96 112 9 10.3 10 10.5 10.2 3.7466 64 65 68 45 116 150 96 112 9 10.3 10 10.5 10.2 3.74

58 5 10.3 9.5 10.5 9.7 3.5662 60 61 64 42 108 140 90 105 7 10.3 9.5 10.5 9.7 3.5663 61 62 65 42 110 142 91 106 8 10.3 9.5 10.5 9.7 3.5665 63 64 67 44 113 146 94 110 8 10.3 9.8 10.5 10 3.6766 64 65 68 45 116 150 96 112 8 10.3 10 10.5 10.2 3.7467 65 65 69 42 113 139 94 111 9 10.3 10 10.6 10.3 3.7868 66 66 70 42 114 141 97 113 7 10.3 10 10.6 10.3 3.7867 65 64 69 42 113 139 97 113 6 10.3 10 10.6 10.3 3.7864 62 59 60 65 67 43 111 137 95 110 5 10.3 10 10.6 10.3 3.7861 59 56 57 62 64 41 105 130 90 105 5 10.3 10 10.6 10.3 3.7858 56 54 53 59 61 40 104 128 86 100 5 10.3 10 10.6 10.3 3.7854 52 50 49 55 57 38 98 121 80 93 3 10.3 10 10.6 10.3 3.78

26 27

Fig. 6.32 curve numberGrain in "C"

Nu w

max

0.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.10.33 0.10.33 0.10.33 0.10.33 0.10.33 0.10.33 0.10.33 0.10.33 0.10.33 0.10.33 0.10.33 0.10.33 0.10.33 0.10.33 0.10.33 0.10.33 0.10.33 0.10.33 0.10.33 0.10.33 0.10.33 0.10.33 0.10.33 0.10.33 0.10.33 0.10.33 0.10.33 0.1

26 27


Nu w

max0.33 0.10.33 0.1

###0.33 0.1010.33 0.1010.33 0.10.33 0.10.33 0.10.33 0.10.33 0.10.33 0.10.33 0.10.33 0.10.33 0.10.33 0.10.33 0.10.33 0.10.33 0.1

###0.33 0.0980.33 0.0980.33 0.0980.33 0.0980.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.101

26 27


Nu w

max0.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.101

26 27


Nu w

max0.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.101

###0.33 0.1010.33 0.1010.33 0.1010.33 0.101

###0.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.101

###0.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.1010.33 0.101

Documents

AA-SM-000 Aluminum Material Data