Buckling test results and preliminary test and analysis correlation from the 8-foot-diameter orthogrid-stiffened cylinder test article TA02 : test dates: 3-6 February 2009 /

Bibliographic Details

Main Author:	Hilburger, Mark W. (Mark William) (Author)
Format:	Government Document eBook
Language:	English
Published:	Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, March 2017.
Series:	NASA technical publication ; 2017-219587.
Subjects:	Buckling. Compression loads. Cylindrical shells. Launch vehicles. Aluminum alloys.
Online Access:	https://purl.fdlp.gov/GPO/gpo82549 http://purl.fdlp.gov/GPO/gpo82549