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Progressive Damage Analysis of Laminated Composite (PDALC) [microform]: (A Computational Model Implemented in the NASA COMET Finite Element Code) Version 2.0

Timothy W. Coats ... [et al.]
Format
Book; Government Document; Microform
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
Language
English
Variant Title
Computational model implemented in the NASA COMET finite element code, version 2.0
Series
NASA/TM
NASA Technical Memorandum
SuDoc Number
NAS 1.15:208718
Description
1 v.
Notes
Shipping list no.: 99-0559-M.
Reproduction Notes
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1999] 1 microfiche.
Series Statement
NASA/TM ; 1998-208718
NASA technical memorandum 208718
Technical Details
  • Access in Virgo Classic
  • Staff View

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    a| Progressive damage analysis of laminated composite (PDALC) h| [microform] : b| (a computational model implemented in the NASA COMET finite element code) version 2.0 / c| Timothy W. Coats ... [et al.].
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    a| Computational model implemented in the NASA COMET finite element code, version 2.0
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    a| 2
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    7
    a| Laminates. 2| nasat
    650
      
    7
    a| Fiber composites. 2| nasat
    650
      
    7
    a| Residual strength. 2| nasat
    650
      
    7
    a| Damage assessment. 2| nasat
    650
      
    7
    a| Finite element method. 2| nasat
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    7
    a| Structural analysis. 2| nasat
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    7
    a| Failure analysis. 2| nasat
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    a| Fracture mechanics. 2| nasat
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