TY  - BOOK
AU  - Abel,Irving
ED  - National Aeronautics and Space Administration. NASA.
TI  - Research and applications in structures at the Nasa Langley Research Center /  
PY  - 1997///
CY  - Hampton : 
PB  - NASA, 
KW  - CARGA DE COMPRESION
KW  - MATERIALES COMPUESTOS
KW  - PANELES COMPUESTOS
KW  - RESISTENCIA RESIDUAL
KW  - DAÑOS POR IMPACTO
KW  - FATIGA
KW  - PLACAS COMPUESTAS
KW  - POLIMEROS DE ALTO RENDIMIENTO
KW  - DISEÑO DE FUSELAJES
KW  - DISEÑO DE ESTRUCTURAS DE AVIONES
KW  - ANALISIS DE FALLAS
KW  - ESTRUCTURAS COMPUESTAS LAMINADAS
KW  - TENSION AXIAL
KW  - PANELES SANDWICH
KW  - PLACAS SANDWICH
KW  - PANELES LATERALES COMPUESTOS
KW  - PLACAS CURVAS
KW  - PANDEO
KW  - ALA COMPUESTA
KW  - ANALISIS NO LINEAL
N1  - NASA Technical Memorandum 110311
N2  - 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
ER  -