Abel, Irving.

Research and applications in structures at the Nasa Langley Research Center / Irving Abel. - Hampton : NASA, 1997.

NASA Technical Memorandum 110311.

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.


CARGA DE COMPRESION
MATERIALES COMPUESTOS
PANELES COMPUESTOS
RESISTENCIA RESIDUAL
DAŅOS POR IMPACTO
FATIGA
PLACAS COMPUESTAS
POLIMEROS DE ALTO RENDIMIENTO
DISEŅO DE FUSELAJES
DISEŅO DE ESTRUCTURAS DE AVIONES
ANALISIS DE FALLAS
ESTRUCTURAS COMPUESTAS LAMINADAS
TENSION AXIAL
PANELES SANDWICH
PLACAS SANDWICH
PANELES LATERALES COMPUESTOS
PLACAS CURVAS
PANDEO
ALA COMPUESTA
ANALISIS NO LINEAL

539.3