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1980 Ford F-250/
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Two stress-strain test results are displayed, showing material properties under load.
Date 1 2/22/2007 Stress in Psi 787473 70000E 60000E 200002 10000-2 404; 50000-: 40000E 30000-f Operator 1 Graeme %Ext.1110.5 1% Offset @02 1 I I | I I 0.00001 0.05000 0.10000 0.15000 0.20000 0.20000 0.30000 0.351000 0.40000 0.40100 Strain ( lu ) Stress/Strain . ' Analyse Curve HELP New Exel Report L Append Exel Report lCursr Cursor 503570349105 l + _1 _ _. Rectanls 11L;otfsetYLg-tbf11_ 0150431 ExtYS(ps_i)1 offset vs (psi)! .. 1. 9 a? Operator Input 128430 117820 119825 178572 154790 149249 F1na| Gage Length] a 0.00000 amgle g 10b #21 0/0 Elong.1 % RA! Area1 0.36183 final area inChS 15-1 Scwwph -100.00 100.00 Gage Lenghl 2-00000 '"Ches g0.00000 Date1 Operator 2122/2007 Graeme % Ext. 165 1% Offset 1% 0.2 ~ 81103=_ Close i 700003 Stress/Strain 1 60000: Analyse Flurtle E 500005 HELP '5 400003 New Exel Report 5 - U _ 3 300005 Append Exel Report 20000-2 100003 D: I I I I l l l l I I 0.00000 0.05000 0.10000 0.15000 0.20000 0.25000 0.30000 0.35000 0.40000 0.47400 -2: Strain (/o) . 7., _ ursor 00503221619 5160'56750T2000 554 ., . hetfiiefw'Eiteh" . OffsetYLglbf- ,UTS(psi)1 ExtYS(psi)1 offsetYS(psl)1 , 9 .p-e. , Operator Input 10 120085 181048 154791 10 Final Gage Length1 0.00000 5 3 # _._JJb #1 % Elong.1 % RA _1Area 036657 ., _ nal area Winohesv Z- 2 _ .0 000 inches .1 Sample a 100.00 100.00 Gage Lengthl 2 0 0.00000
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