Research and applications in structures at the Nasa Langley Research Center /
Automated fabrication technologies for high performance polymer composites. M. J. Shuart, N. J. Johnston, H. B. Dexter, J. M. Marchello, R. W. Grenoble. - A review of the NASA textile composite research. C. C. Poe, H. B. Dexter, I. S. Raju - Design-oriented analysis of aircraft fuselage structures....
Guardado en:
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| Autor Corporativo: | |
| Formato: | Libro |
| Lenguaje: | Inglés |
| Publicado: |
Hampton :
NASA,
1997.
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| Materias: | |
| Aporte de: | Registro referencial: Solicitar el recurso aquí |
| LEADER | 03785Cam#a22004335a#4500 | ||
|---|---|---|---|
| 001 | INGC-MON-019833 | ||
| 003 | AR-LpUFI | ||
| 005 | 20240604172157.0 | ||
| 008 | 190401s1997||||xxu|||||||||||||||||eng d | ||
| 040 | |a AR-LpUFI |b spa |c AR-LpUFI | ||
| 080 | |a 539.3 | ||
| 100 | 1 | |a Abel, Irving. |9 306816 | |
| 245 | 1 | 0 | |a Research and applications in structures at the Nasa Langley Research Center / |c Irving Abel. |
| 260 | |a Hampton : |b NASA, |c 1997. | ||
| 500 | |a NASA Technical Memorandum 110311. | ||
| 520 | 2 | |a Automated fabrication technologies for high performance polymer composites. M. J. Shuart, N. J. Johnston, H. B. Dexter, J. M. Marchello, R. W. Grenoble. - A review of the NASA textile composite research. C. C. Poe, H. B. Dexter, I. S. Raju - Design-oriented analysis of aircraft fuselage structures. AIAA-98-1749. Gary L. Giles - Evaluation of a progressive failure analysis methodology for laminated composite structures. AIAA paper 97-1187. David W. Sleigh, Norman F. Knight, John T. Wang. - Response of composite fuselage sandwich side panels subjected to internal pressure and axial tension. AIAA paper No. 98-1708. Marshal Rouse, Damodar Ambur, Bernard Dopker, Bharat Shah - Damage caracteristics and residual strenght of composite sandwich panels impacted with and without compression loading. AIAA paper No. 98-1783. David M. McGowan, Damodar R. Ambur - Behavior of compression-loaded composite panels with stringer terminations and impact damage. AIAA paper No. 98-1795-CP. Dawn C. Jegley - Fatigue life methodology for tapered composite flexbeam laminates. Gretchen B. Murri, T. Kevin O´Brien, Carl Q. Rousseau - Effect of curvature on the impact damage characteristics and residual strenght of composite plates. AIAA paper No. 98-1881. Damodar R. Amur, James H. Starnes - Fracture mechanics analysis of stitched stiffener-skin debonding. AIAA 98-2022. E. H. Glaessgen, I. S. Raju, C. C. Poe - Development of curved-plate elements for the exact buckling analysis of composite plate assemblies including transverse shear effects. David M. McGowan, Melvin S. Anderson - Application of interface technology in nonlinear analysis of a stitched/rfi composite wing stub box. John T. Wang, Jonathan B. Ransom - Experimental investigation of a graphite-composite intertank section for a reusable launc vehicle. James Wayne Sawyer, Harold Bush - Buckling analysis of anisotropic curved panels and shells with variable curvature. AIAA paper 98-1772. Navin Jaunky, Norman F. Knight, Damodar R. Ambur - Anomalous buckling characteristics of laminated metal-matrix composite plates wiyh central square holes. NASA/TP 1998-206559. William L. Ko - The NASA monographs on shell stability design recommendations. A review and suggested improvements. NASA/TP 1998-206290. Michael P. Nemeth, James H. Starnes. | |
| 650 | 4 | |a CARGA DE COMPRESION |9 306817 | |
| 650 | 4 | |a MATERIALES COMPUESTOS |9 264975 | |
| 650 | 4 | |a PANELES COMPUESTOS |9 306818 | |
| 650 | 4 | |a RESISTENCIA RESIDUAL |9 288400 | |
| 650 | 4 | |a DAÑOS POR IMPACTO |9 306819 | |
| 650 | 4 | |a FATIGA |9 264838 | |
| 650 | 4 | |a PLACAS COMPUESTAS |9 306820 | |
| 650 | 4 | |a POLIMEROS DE ALTO RENDIMIENTO |9 306821 | |
| 650 | 4 | |a DISEÑO DE FUSELAJES |9 306822 | |
| 650 | 4 | |a DISEÑO DE ESTRUCTURAS DE AVIONES |9 306823 | |
| 650 | 4 | |a ANALISIS DE FALLAS |9 275591 | |
| 650 | 4 | |a ESTRUCTURAS COMPUESTAS LAMINADAS |9 306824 | |
| 650 | 4 | |a TENSION AXIAL |9 306825 | |
| 650 | 4 | |a PANELES SANDWICH |9 284014 | |
| 650 | 4 | |a PLACAS SANDWICH |9 306826 | |
| 650 | 4 | |a PANELES LATERALES COMPUESTOS |9 306827 | |
| 650 | 4 | |a PLACAS CURVAS |9 286798 | |
| 650 | 4 | |a PANDEO |9 264645 | |
| 650 | 4 | |a ALA COMPUESTA |9 306828 | |
| 650 | 4 | |a ANALISIS NO LINEAL |9 286765 | |
| 710 | |a National Aeronautics and Space Administration. NASA. |9 289258 | ||
| 942 | |c LIB |2 ddc |6 _ | ||
| 999 | |c 19832 |d 19832 | ||