Response of composite fuselage sandwich side panels subjected to internal pressure and axial tension
By: Marshall Rouse ... [et al.].
Contributors: Rouse, Marshall.; United States. National Aeronautics and Space Administration.
Series: NASA/TM -- 208191.; NASA technical memorandum -- 208191.
Publisher: National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1998
Place of publication: [Washington, D.C; Springfield, Va
Language: eng
Format: Microform
Subjects: Composite structures.; Fuselages.; Sandwich structures.; Axial loads.; Internal pressure.; Load tests.; Panels.; Structural analysis.; Finite element method.; Tensile deformation.; Critical loading.
Notes: Shipping list no.: 98-1060-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1998] 1 microfiche.