Damage characteristics and residual strength of composite sandwich 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
Notes: Also issued as NASA TM 208122 on shipping list no.: 99-0385-M.

Shipping list no.: 99-0032-M.

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