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200 1 $aGradiente, rotore, divergenza$fEnzo Tonti.
210   $aMIlano$cTamburini$d1972
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200 10$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.
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615  7$aPressure ratio.
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702   $aRe$b Richard J.
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