LEADER 01776oam  2200481   450 
001 9910709978403321
005 20180824073246.0
035   $a(CKB)5470000002474480
035   $a(OCoLC)1049569652
035   $a(OCoLC)995470000002474480
035   $a(EXLCZ)995470000002474480
100   $a20180823j198502    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aStatic internal performance of a two-dimensional convergent nozzle with thrust-vectoring capability up to 60 ?/$fLaurence D. Leavitt
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration, Scientific and Technical Information Branch,$dFebruary 1985.
215   $a1 online resource (66 pages) $cillustrations
225 1 $aNASA/TP ;$v2391
300   $a"February 1985."
320   $aIncludes bibliographical references (pages 7-8).
606   $aConvergent$2nasat
606   $aThrust vector control$2nasat
606   $aWind tunnel tests$2nasat
606   $aNozzle flow$2nasat
606   $aTransonic wind tunnels$2nasat
615  7$aConvergent.
615  7$aThrust vector control.
615  7$aWind tunnel tests.
615  7$aNozzle flow.
615  7$aTransonic wind tunnels.
700   $aLeavitt$b Laurence D.$01394871
712 02$aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Branch,
712 02$aLangley Research Center.
801  0$bGPO
801  1$bGPO
801  2$bGPO
906   $aBOOK
912   $a9910709978403321
996   $aStatic internal performance of a two-dimensional convergent nozzle with thrust-vectoring capability up to 60 ?$93452729
997   $aUNINA