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181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aThermostructural behavior of a hypersonic aircraft sandwich panel subjected to heating on one side /$fWilliam L. Ko
210  1$a[Washington, D.C.] :$cNational Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program,$dApril 1997.
215   $a1 online resource (iii, 47 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v4769
300   $aTitle from title screen (viewed March 2, 2016).
300   $a"April 1997."
300   $a"Performing organization: NASA Dryden Flight Research Center , Edwards, California"--Report documentation page.
320   $aIncludes bibliographical references (page 12).
606   $aAerodynamic heating$2nasat
606   $aAircraft structures$2nasat
606   $aHeat sinks$2nasat
606   $aHoneycomb cores$2nasat
606   $aThermal stresses$2nasat
615  7$aAerodynamic heating.
615  7$aAircraft structures.
615  7$aHeat sinks.
615  7$aHoneycomb cores.
615  7$aThermal stresses.
700   $aKo$b William L.$01388928
712 02$aHugh L. Dryden Flight Research Center.
712 02$aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Program,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
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906   $aBOOK
912   $a9910704381103321
996   $aThermostructural behavior of a hypersonic aircraft sandwich panel subjected to heating on one side$93529366
997   $aUNINA