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100   $a20100527d1985      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aStatic internal performance of a single-engine nonaxisymmetric-nozzle vaned-thrust-reverser design with thrust modulation capabilities$b[electronic resource] /$fLaurence D. Leavitt and James R. Burley II
210  1$a[Washington, D.C.] :$cNational Aeronautics and Space Administration, Scientific and Technical Information Branch,$d1985.
215   $a1 online resource (106 pages) $cdigital, PDF file
225 1 $aNASA technical paper ;$v2519
300   $aTitle from title screen (viewed May 26, 2010).
320   $aIncludes bibliographical references (pages 14-15).
410  0$aNASA technical paper ;$v2519.
606   $aNozzle geometry$2nasat
606   $aStatic tests$2nasat
606   $aThrust reversal$2nasat
606   $aWind tunnel tests$2nasat
615  7$aNozzle geometry.
615  7$aStatic tests.
615  7$aThrust reversal.
615  7$aWind tunnel tests.
700   $aLeavitt$b Laurence D$01394871
701   $aBurley$b James R$01415166
712 02$aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Branch.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910697180503321
996   $aStatic internal performance of a single-engine nonaxisymmetric-nozzle vaned-thrust-reverser design with thrust modulation capabilities$93516390
997   $aUNINA