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Local strain redistribution corrections for a simplified inelastic analysis procedure based on an elastic finite-element analysis / / Albert Kaufman and Shoi Y. Hwang
| Local strain redistribution corrections for a simplified inelastic analysis procedure based on an elastic finite-element analysis / / Albert Kaufman and Shoi Y. Hwang |
| Autore | Kaufman Albert <1928-> |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , March 1985 |
| Descrizione fisica | 1 online resource (11 pages) : illustrations |
| Collana | NASA/TP |
| Soggetto topico |
Aircraft gas-turbines - Materials
Elastic analysis (Engineering) Finite element method Strains and stresses Cyclic loads Inelastic stress Nonlinear equations Stress distribution Stress-strain relationships |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910709797103321 |
Kaufman Albert <1928->
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| Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , March 1985 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Nonlinear damage analysis- postulate and evaluation / / B.N. Leis and T.P. Forte
| Nonlinear damage analysis- postulate and evaluation / / B.N. Leis and T.P. Forte |
| Autore | Leis B. N. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , March 1983 |
| Descrizione fisica | 1 online resource (90 pages) : illustrations |
| Collana | NASA/CR |
| Soggetto topico |
Damage assessment
Fatigue life Copper Residual stress Inelastic stress |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910709748303321 |
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Leis B. N.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , March 1983 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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