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100   $a20111115j198012    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aEffects of sidewall geometry on the installed performance of nonaxisymmetric convergent-divergent exhaust nozzles /$fJeffery A. Yetter, Laurance D. Leavitt
210  1$a[Washington, D.C.] :$cNational Aeronautics and Space Administration, Scientific and Technical Information Branch,$dDecember 1980.
215   $a1 online resource (116 pages) $cillustrations
225 1 $aNASA technical paper ;$v1771
300   $aTitle from title screen (viewed on Aug. 19, 2016).
300   $a"December 1980."
300   $a"Performing Organization: NASA Langley Research Center"--Report documentation page.
320   $aIncludes bibliographical references (pages 18-19).
606   $aConvergent-divergent nozzles$2nasat
606   $aExhaust flow simulation$2nasat
606   $aNozzle design$2nasat
606   $aStatic pressure$2nasat
606   $aWind tunnel tests$2nasat
615  7$aConvergent-divergent nozzles.
615  7$aExhaust flow simulation.
615  7$aNozzle design.
615  7$aStatic pressure.
615  7$aWind tunnel tests.
700   $aYetter$b Jeffery A.$01419448
702   $aLeavitt$b Laurence D.
712 02$aLangley Research Center.
712 02$aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Branch,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bOCLCO
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910707455003321
996   $aEffects of sidewall geometry on the installed performance of nonaxisymmetric convergent-divergent exhaust nozzles$93533934
997   $aUNINA