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100   $a20111114j198011    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aIn-flight boundary-layer measurements on a hollow cylinder at a Mach number of 3.0 /$fRobert D. Quinn and Leslie Gong
210  1$a[Washington, D.C.] :$cNational Aeronautics and Space Administration, Scientific and Technical Information Branch,$dNovember1980.
215   $a1 online resource (49 pages) $cillustrations
225 1 $aNASA technical paper ;$v1764
300   $aTitle from title screen (viewed on Aug. 18, 2016).
300   $a"November1980."
300   $a"Performing Organization: NASA Dryden Flight Research Center"--Report documentation page.
320   $aIncludes bibliographical references (pages 18-19).
606   $aHeat transfer coefficients$2nasat
606   $aMach number$2nasat
606   $aReynolds number$2nasat
606   $aShear flow$2nasat
615  7$aHeat transfer coefficients.
615  7$aMach number.
615  7$aReynolds number.
615  7$aShear flow.
700   $aQuinn$b Robert D.$0142872
702   $aGong$b Leslie
712 02$aHugh L. Dryden Flight Research Center.
712 02$aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Branch,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bOCLCF
801  2$bOCLCQ
801  2$bOCLCO
801  2$bGPO
906   $aBOOK
912   $a9910707458403321
996   $aIn-flight boundary-layer measurements on a hollow cylinder at a Mach number of 3.0$93474760
997   $aUNINA