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100   $a20120408j197904    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aOnset of condensation effects with an NACA 0012-64 airfoil tested in the Langley 0.3-meter transonic cryogenic tunnel /$fRobert M. Hall
210   $a[Washington, D.C.] $cNational Aeronautics and Space Administration, Scientific and Technical Information Office$dApril 1979
215   $a1 online resource (69 pages) $cillustrations
225 1 $aNASA technical paper ;$v1385
300   $aTitle from title screen (viewed on Aug. 10, 2016).
300   $a"April 1979."
300   $a"Performing Organization: NASA Langley Research Center"--Report documentation page.
320   $aIncludes bibliographical references (pages 22-23).
606   $aAirfoils$2nasat
606   $aCryogenic wind tunnels$2nasat
606   $aPressure distribution$2nasat
606   $aStagnation temperature$2nasat
606   $aSupercooling$2nasat
615  7$aAirfoils.
615  7$aCryogenic wind tunnels.
615  7$aPressure distribution.
615  7$aStagnation temperature.
615  7$aSupercooling.
700   $aHall$b Robert M.$0157258
712 02$aLangley Research Center.
712 02$aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Office,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bOCLCF
801  2$bOCLCQ
801  2$bOCLCO
801  2$bGPO
906   $aBOOK
912   $a9910707490903321
996   $aOnset of condensation effects with an NACA 0012-64 airfoil tested in the Langley 0.3-meter transonic cryogenic tunnel$93488837
997   $aUNINA