A numerical study on the effect of facesheet-core disbonds on the buckling load of curved honeycomb sandwich panels /

Bibliographic Details
Main Author:	Pineda, Evan J. (Author)
Corporate Author:	United States. National Aeronautics and Space Administration (sponsoring body.)
Format:	Government Document eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, August 2015.
Series:	NASA technical memorandum ; 2015-218861.
Subjects:	Spacecraft shielding. Curved panels. Honeycomb cores. Debonding (materials) Heavy lift launch vehicles.
Online Access:	https://purl.fdlp.gov/GPO/gpo63968 http://purl.fdlp.gov/GPO/gpo63968

Description
Item Description:	Title from title screen (viewed on Jan. 6, 2016). "August 2015." "Prepared for the 30th Annual Technical Conference sponsored by the American Society for Composites, East Lansing, Michigan, September 28-30, 2015." "Paper no. 1713."
Physical Description:	1 online resource (18 pages) : color illustrations.
Bibliography:	Includes bibliographical references (pages 16-18).