Item Details

Compression Behavior of Graphite-Thermoplastic and Graphite-Epoxy Panels With Circular Holes or Impact Damage

Dawn C. Jegley
Format
Book; Government Document; Online; EBook
Published
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1991.
Language
English
Series
NASA Technical Paper
Description
15 p. : ill. ; 28 cm.
Mode of access: Internet.
Notes
  • Prepared at Langley Research Center.
  • Bibliography: p. 12.
Series Statement
NASA technical paper ; 3071
Logo for No Copyright - United StatesNo Copyright - United States
Technical Details

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    a| Compression behavior of graphite-thermoplastic and graphite-epoxy panels with circular holes or impact damage / c| Dawn C. Jegley.
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    a| Bibliography: p. 12.
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    a| Epoxy resins.
    650
      
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    a| Graphite fibers.
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    a| Airplanes x| Materials x| Testing.
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    a| Plates (Engineering)
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    a| Composite materials x| Testing.
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    a| Materials x| Compression testing.
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