Research Catalog

Response of composite panels with stiffness gradients due to stiffener terminations and cutouts

Title
Response of composite panels with stiffness gradients due to stiffener terminations and cutouts [microform] / Damodar R. Ambur ... [et al.].
Publication
[Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]

Details

Additional Authors
  • Ambur, Damodar R.
  • United States. National Aeronautics and Space Administration.
Description
1 v.
Uniform Title
NASA technical memorandum ; 112845.
Subject
  • Composite structures
  • Aircraft structures
  • Graphite-epoxy composites
  • Failure modes
  • Finite element method
  • Stiffening
Note
  • Shipping list no.: 98-0599-M.
Reproduction (note)
  • Microfiche.
Call Number
READEX Microfiche NAS 1.15:112845
OCLC
marcive40431870
Title
Response of composite panels with stiffness gradients due to stiffener terminations and cutouts [microform] / Damodar R. Ambur ... [et al.].
Imprint
[Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
Series
NASA technical memorandum ; 112845.
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 1 microfiche. (NASA-TM ; 112845).
Added Author
Ambur, Damodar R.
United States. National Aeronautics and Space Administration.
Gpo Item No.
0830-D (MF)
Sudoc No.
NAS 1.15:112845
Research Call Number
READEX Microfiche NAS 1.15:112845
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