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100   $a20120408j198012    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aInvestigation of convergent-divergent nozzles applicable to reduced-power supersonic cruise aircraft /$fBobby L. Berrier and Richard J. Re
210  1$a[Washington, D.C.] :$cNational Aeronautics and Space Administration, Scientific and Technical Information Branch,$dDecember 1980.
215   $a1 online resource (215 pages) $cchiefly illustrations
225 1 $aNASA technical paper ;$v1766
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 (page 23).
606   $aConvergent-divergent nozzles$2nasat
606   $aMach number$2nasat
606   $aNozzle design$2nasat
606   $aPerformance tests$2nasat
606   $aPressure ratio$2nasat
615  7$aConvergent-divergent nozzles.
615  7$aMach number.
615  7$aNozzle design.
615  7$aPerformance tests.
615  7$aPressure ratio.
700   $aBerrier$b Bobby L.$01389747
702   $aRe$b Richard J.
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$bOCLCQ
801  2$bOCLCF
801  2$bOCLCQ
801  2$bOCLCO
801  2$bGPO
906   $aBOOK
912   $a9910707455903321
996   $aInvestigation of convergent-divergent nozzles applicable to reduced-power supersonic cruise aircraft$93545765
997   $aUNINA