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NASA Technical Reports Server (NTRS) 20060026045: Damage Tolerance Analysis of Space Shuttle External Tank Lug Fillet Welds Using NASGRO PDF

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Preview NASA Technical Reports Server (NTRS) 20060026045: Damage Tolerance Analysis of Space Shuttle External Tank Lug Fillet Welds Using NASGRO

Source of Acquisition NASA Marshall Space Flight Center Damage Tolerance Analysis of Space Shuttle External Tank Lug Fillet Welds Using NASGRO Abstract The damage tolerance of the External Tank (ET) lug welds were reassessed because of an increase in the loads due to the removal of the protuberance air load (PAT.,) ramp. The analysis methods included detailed finite element analysis (FEA) of the ET welded lugs and FEA of the lug weld test configuration. The FEA results were used as input to the crack growth analysis code NASGRO to calculate the mission life capability of the ET lug welds and to predict the number of cycles to failure in the lug weld testing. The presentation presents the method of transferring the FEM results to the NASGRO model and gives correlations between FEM and NASGRO stress intensity calculations. II 0 , / / i \ \ .- + a, Y 5 K e m -5 S E rn . S 0 .I CTS L 3 ZT) G= s S 3 I e a, v) e v) a, e e -a, 12 .- m -I - LL 3 t- W +- e co W L S a, 8 .0I E a, a. 3 .u- m cn .0- i-r of 0 ([I i-r S 0 0 s m w s i-r v) S 3 LL E c3 a a, m c--a, a a, I 51 a, m -a 0 .7-3 0 .P- ) .m- L cn a, a, \/ 0 . 0 0 -5 c E a v) U a M cu 0 L 0 v % 0 2 7 W LL E 0 t: cn 6 U a, m .cnI IP L - +3-J % I * 0 m m 2 ts 0 t rc a, U LL 0 + 0 m + a b a, m m 9 Y- d 0 m m cn a, _0sc 0m T- o + 0 %k U LL c 0 0s 0 3 F 0 N 5 a t- u b t- a3 t W a F N N e E V c e m T I a, 0 S cI5 -til P - Y El= a @ I 9 9 9 4 9 9 9 9 9 9 9 9 9 S L 0 000000000000 -I r-" y o9o9o9o9o9o9o9o4o9o9 o9 o9 o9 U J . a , 0 S as -5 0 I- a, L g c I I cn .0cI E" 0 m u, 0" m a , . . 0 s A I - .- LL I- u-l

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