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100   $a20170202j199303    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aCharacterization of cavity flow fields using pressure data obtained in the Langley 0.3-meter transonic cryogenic tunnel /$fM.B. Tracy and E.B. Plentovich
210  1$a[Washington, D.C.] :$cNational Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program,$dMarch 1993.
215   $a1 online resource (32 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v4436
300   $a"March 1993" Report documentation page.
300   $a"Performing organization: NASA Langley Research Center"--Report documentation page.
320   $aIncludes bibliographical references (pages 6-7).
606   $aCavity flow$2nasat
606   $aPressure distribution$2nasat
606   $aTransonic speed$2nasat
606   $aUnsteady flow$2nasat
606   $aYaw$2nasat
615  7$aCavity flow.
615  7$aPressure distribution.
615  7$aTransonic speed.
615  7$aUnsteady flow.
615  7$aYaw.
700   $aTracy$b M. B.$01405255
702   $aPlentovich$b Elizabeth B.
712 02$aLangley Research Center.
712 02$aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Program,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910707953203321
996   $aCharacterization of cavity flow fields using pressure data obtained in the Langley 0.3-meter transonic cryogenic tunnel$93481379
997   $aUNINA