LEADER 01924oam  2200493   450 
001 9910704380903321
005 20160302141918.0
035   $a(CKB)5470000002439873
035   $a(OCoLC)777248062
035   $a(EXLCZ)995470000002439873
100   $a20120213j199612    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aThermal and mechanical buckling analysis of hypersonic aircraft hat-stiffened panels with varying face sheet geometry and fiber orientation /$fWilliam L. Ko
210  1$a[Washington, D.C.] :$cNational Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program,$dDecember 1996.
215   $a1 online resource (v, 30 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v4770
300   $aTitle from title screen (viewed March 2, 2016).
300   $a"December 1996."
320   $aIncludes bibliographical references (page 15).
606   $aAircraft structures$2nasat
606   $aThermal buckling$2nasat
606   $aMechanical properties$2nasat
606   $aFinite element method$2nasat
606   $aHypersonic aircraft$2nasat
615  7$aAircraft structures.
615  7$aThermal buckling.
615  7$aMechanical properties.
615  7$aFinite element method.
615  7$aHypersonic aircraft.
700   $aKo$b William L.$01388928
712 02$aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Program,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bOCLCO
801  2$bGPO
906   $aBOOK
912   $a9910704380903321
996   $aThermal and mechanical buckling analysis of hypersonic aircraft hat-stiffened panels with varying face sheet geometry and fiber orientation$93466184
997   $aUNINA