Correlation of structural analysis and test results for the McDonnell Douglas stitched/RFI all-composite wing stub box /

Bibliographic Details

Main Author:	Wang, John T. (Author)
Format:	Government Document eBook
Language:	English
Published:	Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, July 1996.
Series:	NASA technical memorandum ; 110267.
Subjects:	Composite structures. Finite element method. Graphite-epoxy composites. Wings. Strain distribution. Bending. Commercial aircraft. Aircraft structures.
Online Access:	https://purl.fdlp.gov/GPO/gpo75304