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Compression behavior of graphite-thermoplastic and graphite-epoxy panels with circular holes or impact damage /
Dawn C. Jegley.



Main Author: Jegley, Dawn C.
Language(s): English
Published: Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; 1991.
Subjects: Epoxy resins.
Graphite fibers.
Airplanes > Airplanes / Materials > Airplanes / Materials / Testing.
Plates (Engineering)
Composite materials > Composite materials / Testing.
Materials > Materials / Compression testing.
Note: Prepared at Langley Research Center.
Physical Description: 15 p. : ill. ; 28 cm.
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