A numerical study on the effect of facesheet-core disbonds on the buckling load of curved honeycomb sandwich panels / Evan J. Pineda [and three others]

Saved in:

Bibliographic Details
Online Access:	Online Access Online Access
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.

Internet

Online Access
Online Access

Holdings details from Online
Call Number:	NAS 1.15:2015-218861
NAS 1.15:2015-218861	Available