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

An edition of Design, optimization, and evaluation of A1-2139 compression panel with integral T-stiffeners (2012)

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

By Sameer B. Mulani

0 (0 Ratings)

0 Want to read0 Currently reading0 Have read

Publish Date

2012

Publisher

National Aeronautics and Space Administration, Langley Research Center

Language

eng

Pages

Description:

subjects: Design optimization, Finite element method, Photogrammetry, Aluminum alloys, Digital systems, Displacement, Buckling