Damage characteristics and residual strength of composite sandwaich panels impacted with and without compression loading
Subtitle: presented at the 39th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, session no. 15--damage tolerance : Long Beach, California, April 20-23, 1998
By: David M. McGowan and Damodar R. Ambur.
Contributors: Ambur, Damodar R.; United States. National Aeronautics and Space Administration.; AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference (1998 Long Beach, Calif.)
Series: AIAA paper -- no. 98-1783.; NASA/TM -- 1998-207691.; NASA technical memorandum -- 207691.
Publisher: National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1998
Place of publication: [Washington, DC; Springfield, Va
Language: eng
Format: Microform
Subjects: Composite structures.; Impact damage.; Panels.; Residual strength.; Sandwich structures.; Compression loads.; Impact tests.; Failure analysis.; Structural analysis.
Notes: Shipping list no.: 99-0032-M.

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