Design, optimization, and evaluation of A1-2139 compression panel with integral T-stiffeners
By: Sameer B. Mulani ... [et al.].
Contributors: Langley Research Center
Series: NASA/TP -- 2012-217584; NASA technical paper -- 2012-217584
Publisher: National Aeronautics and Space Administration, Langley Research Center
Published: 2012
Place of publication: Hampton, Va
Language: eng
Format: [electronic resource] /
Number of pages: 33
Subjects: Design optimization; Finite element method; Photogrammetry; Aluminum alloys; Digital systems; Displacement; Buckling
Notes: Title from title screen (viewed on Nov. 13, 2012).

"June 2012."

Includes bibliographical references (p. 20-22).

Sponsored by National Aeronautics and Space Administration 561581.02.08.07.43.01

L-20156