Design, optimization, and evaluation of integrally-stiffened Al-2139 panel with curved stiffeners /

Bibliographic Details

Corporate Author:	Langley Research Center
Other Authors:	Havens, David
Format:	Government Document eBook
Language:	English
Published:	Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2011]
Series:	NASA technical memorandum ; 217308.
Subjects:	Design optimization. Load tests. Tolerances (mechanics) Panels. Stiffening. Curvature. Loads (forces)
Online Access:	https://purl.fdlp.gov/GPO/gpo22684