Finite element analysis and test results comparison for the hybrid wing body center section test article /

Bibliographic Details

Main Author:	Przekop, Adam (Author)
Format:	Government Document eBook
Language:	English
Published:	Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, April 2016.
Series:	NASA technical memorandum ; 2016-218973.
Subjects:	Critical loading. Finite element method. Strain measurement. Structural stability. Wings.
Online Access:	https://purl.fdlp.gov/GPO/gpo85619