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035   $a(EXLCZ)995470000002473090
100   $a20120408j198604    ua             0
101 0 $aeng
135   $aurbn||||||abp
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aStatic internal performance of a thrust vectoring and reversing two-dimensional convergent-divergent nozzle with an aft flap /$fRichard J. Re and Laurence D. Leavitt
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration, Scientific and Technical Information Branch,$dApril 1986.
215   $a1 online resource (110 pages) $cillustrations
225 1 $aNASA/TP ;$v2549
300   $a"March 1982."
320   $aIncludes bibliographical references (pages 15-16).
606   $aStatic tests$2nasat
606   $aThrust vector control$2nasat
606   $aThrust reversal$2nasat
606   $aWind tunnel tests$2nasat
606   $aNozzle geometry$2nasat
606   $aJet nozzles
606   $aJet planes$xThrust reversers
606   $aJet nozzles$2fast
606   $aJet planes$xThrust reversers$2fast
615  7$aStatic tests.
615  7$aThrust vector control.
615  7$aThrust reversal.
615  7$aWind tunnel tests.
615  7$aNozzle geometry.
615  0$aJet nozzles.
615  0$aJet planes$xThrust reversers.
615  7$aJet nozzles.
615  7$aJet planes$xThrust reversers.
700   $aRe$b Richard J.$01387323
702   $aLeavitt$b Laurence D.
712 02$aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Branch,
712 02$aLangley Research Center.
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bOCLCO
801  2$bOCLCF
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910709716003321
996   $aStatic internal performance of a thrust vectoring and reversing two-dimensional convergent-divergent nozzle with an aft flap$93542739
997   $aUNINA