000 | 00661nam a2200193 4500 | ||
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005 | 20201005123606.0 | ||
008 | 201005b xxu||||| |||| 00| 0 eng d | ||
040 | _cIIT Kanpur | ||
041 | _aeng | ||
100 | _aStephens, B. Wendell | ||
245 |
_aComputer program for finite-difference solutions of shells of revolution under asymmetric dynamic loading [NASA TN D-6059] _cWendell B. stephens and Martha P. Robinson |
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260 |
_aWashington, D. C. _bNASA _c1971 |
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300 | _a66p | ||
440 | _aNational Aeronautics and Space Administation (NASA) | ||
505 | _atechnical report NASA | ||
650 | _a asymmetric | ||
700 | _aRobinson, P. Martha | ||
942 | _cTR | ||
999 |
_c563402 _d563402 |