Research Catalog

Response of composite fuselage sandwich side panels subjected to internal pressure and axial tension

Title
Response of composite fuselage sandwich side panels subjected to internal pressure and axial tension [microform] / Marshall Rouse ... [et al.].
Publication
[Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1998]

Details

Additional Authors
  • Rouse, Marshall.
  • United States. National Aeronautics and Space Administration.
Description
1 v.
Series Statement
NASA/TM ; 208191
Uniform Title
NASA technical memorandum ; 208191.
Subject
  • Composite structures
  • Fuselages
  • Sandwich structures
  • Axial loads
  • Internal pressure
  • Load tests
  • Panels
  • Structural analysis
  • Finite element method
  • Tensile deformation
  • Critical loading
Note
  • Also issued as NASA TM 208213 on shipping list no.: 98-1059-M.
  • Shipping list no.: 98-1060-M.
Reproduction (note)
  • Microfiche.
Call Number
READEX Microfiche NAS 1.15:208213
OCLC
marcive40386800
Title
Response of composite fuselage sandwich side panels subjected to internal pressure and axial tension [microform] / Marshall Rouse ... [et al.].
Imprint
[Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1998]
Series
NASA/TM ; 208191
NASA technical memorandum ; 208191.
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1998] 1 microfiche.
Added Author
Rouse, Marshall.
United States. National Aeronautics and Space Administration.
Gpo Item No.
0830-D (MF)
Sudoc No.
NAS 1.15:208191
NAS 1.15:208213
Research Call Number
READEX Microfiche NAS 1.15:208213
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