Compression behavior of graphite-thermoplastic and graphite-epoxy panels with circular holes or impact damage

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035 ‡asdr-uiuc6354285
035 ‡a(OCoLC)23333825
040 ‡aABC ‡cABC
049 ‡aUIUU
090 ‡aTL521.3 ‡b.N18 no. 3071
100 1 ‡aJegley, Dawn C.
245 1 0 ‡aCompression behavior of graphite-thermoplastic and graphite-epoxy panels with circular holes or impact damage / ‡cDawn C. Jegley.
260 ‡aWashington, D.C. : ‡bNational Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; ‡aSpringfield, Va. : ‡bFor sale by the National Technical Information Service, ‡c1991.
300 ‡a15 p. : ‡bill. ; ‡c28 cm.
490 0 ‡aNASA technical paper ; ‡v3071
500 ‡aPrepared at Langley Research Center.
504 ‡aBibliography: p. 12.
538 ‡aMode of access: Internet.
650 0 ‡aEpoxy resins.
650 0 ‡aGraphite fibers.
650 0 ‡aAirplanes ‡xMaterials ‡xTesting.
650 0 ‡aPlates (Engineering)
650 0 ‡aComposite materials ‡xTesting.
650 0 ‡aMaterials ‡xCompression testing.
710 2 ‡aLangley Research Center.
CID ‡a011423868
DAT 0 ‡a20100930145803.0 ‡b20141013010000.0
DAT 1 ‡a20141112173021.0 ‡b2018-03-08T19:38:43Z
CAT ‡aSDR-UIUC ‡dUNKNOWN ‡lloader.pl-003-020
FMT ‡aBK
HOL ‡0sdr-uiuc6354285 ‡auiug ‡bSDR ‡cUIUC ‡puiug.30112106711176 ‡sUIU ‡16354285
974 ‡bUIU ‡cUIUC ‡d20180308 ‡sgoogle ‡uuiug.30112106711176 ‡y1991 ‡rpd ‡qbib ‡tUS fed doc--NTIS: pubdate < 2014