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A Progressive Damage Methodology for Residual Strength Predictions of Notched Composite Panels

Timothy W. Coats and Charles E. Harris
Format
EBook; Book; Government Document; Online
Published
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, June 1998.
Language
English
Series
NASA/TM
NASA Technical Memorandum
SuDoc Number
NAS 1.15:207646
Description
1 online resource (43 pages) : illustrations.
Notes
  • "June 1998."
  • "Performing organization: NASA Langley Research Center"--Report documentation page.
  • Includes bibliographical references (pages 22-24).
Series Statement
NASA/TM ; 1998-207646
NASA technical memorandum ; 1998-207646
Copyright Not EvaluatedCopyright Not Evaluated
Technical Details
  • Access in Virgo Classic
  • Staff View

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    a| Hampton, Virginia : b| National Aeronautics and Space Administration, Langley Research Center, c| June 1998.
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    a| text b| txt 2| rdacontent
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    a| "Performing organization: NASA Langley Research Center"--Report documentation page.
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    a| Sponsored by the National Aeronautics and Space Administration d| 538-13-11-05 d| L-17729
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    7
    a| Composite structures. 2| nasat
    650
      
    7
    a| Crack propagation. 2| nasat
    650
      
    7
    a| Epoxy matrix composites. 2| nasat
    650
      
    7
    a| Fractography. 2| nasat
    650
      
    7
    a| Fracture mechanics. 2| nasat
    650
      
    7
    a| Fracture strength. 2| nasat
    650
      
    7
    a| Laminates. 2| nasat
    650
      
    7
    a| Loads (forces) 2| nasat
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    7
    a| Residual strength. 2| nasat
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    a| Harris, Charles E., d| 1950- e| author.
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    a| NASA technical memorandum ; v| 1998-207646.
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