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| LEADER |
03785Cam#a22004335a#4500 |
| 001 |
INGC-MON-019833 |
| 003 |
AR-LpUFI |
| 005 |
20240604172157.0 |
| 008 |
190401s1997||||xxu|||||||||||||||||eng d |
| 040 |
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|a AR-LpUFI
|b spa
|c AR-LpUFI
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| 080 |
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|a 539.3
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| 100 |
1 |
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|a Abel, Irving.
|9 306816
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| 245 |
1 |
0 |
|a Research and applications in structures at the Nasa Langley Research Center /
|c Irving Abel.
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| 260 |
|
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|a Hampton :
|b NASA,
|c 1997.
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| 500 |
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|a NASA Technical Memorandum 110311.
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| 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 |
|
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|c LIB
|2 ddc
|6 _
|
| 999 |
|
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|c 19832
|d 19832
|