Design, optimization, and evaluation of A1-2139 compression panel with integral T-stiffeners /

Bibliographic Details

Corporate Author:	Langley Research Center
Other Authors:	Mulani, Sameer B.
Format:	Government Document eBook
Language:	English
Published:	Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2012]
Series:	NASA technical paper ; 2012-217584.
Subjects:	Design optimization. Finite element method. Photogrammetry. Aluminum alloys. Digital systems. Displacement. Buckling.
Online Access:	https://purl.fdlp.gov/GPO/gpo31180