Research Catalog

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

Title
Design, optimization, and evaluation of A1-2139 compression panel with integral T-stiffeners / Sameer B. Mulani ... [and others].
Publication
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2012]

Available Online

https://purl.fdlp.gov/GPO/gpo31180

Details

Additional Authors
  • Mulani, Sameer B.
  • Langley Research Center.
Description
1 online resource (x, 33 pages) : illustrations (some color).
Series Statement
NASA/TP ; 2012-217584
Uniform Title
NASA technical paper ; 2012-217584.
Subject
  • Design optimization
  • Finite element method
  • Photogrammetry
  • Aluminum alloys
  • Digital systems
  • Displacement
  • Buckling
Note
  • Title from title screen (viewed on Nov. 13, 2012).
  • "June 2012."
Bibliography (note)
  • Includes bibliographical references (pages 20-22).
Funding (note)
  • Sponsored by National Aeronautics and Space Administration
Call Number
GPO Internet NAS 1.60:2012-217584
OCLC
marcive817725601
Title
Design, optimization, and evaluation of A1-2139 compression panel with integral T-stiffeners / Sameer B. Mulani ... [and others].
Publisher
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2012]
Type of Content
text
Type of Medium
computer
Type of Carrier
online resource
Series
NASA/TP ; 2012-217584
NASA technical paper ; 2012-217584.
Bibliography
Includes bibliographical references (pages 20-22).
Funding
Sponsored by National Aeronautics and Space Administration 561581.02.08.07.43.01
L-20156
Connect to:
https://purl.fdlp.gov/GPO/gpo31180
Added Author
Mulani, Sameer B.
Langley Research Center.
Gpo Item No.
0830-H-15 (online)
Sudoc No.
NAS 1.60:2012-217584
View in Legacy Catalog