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100   $a20170126j198410    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aStatic internal performance of single -expansion-ramp nozzles with thrust-vectoring capability up to 60° /$fBobby L. Berrier and Laurence D. Leavitt
210  1$a[Washington, D.C.] :$cNational Aeronautics and Space Administration, Scientific and Technical Information Branch,$dOctober 1984.
215   $a1 online resource (141 pages) $cillustrations
225 1 $aNASA technical paper ;$v2364
300   $a"October 1984" Report documentation page.
300   $a"Performing organization: NASA Langley Research Center" Report documentation page.
320   $aIncludes bibliographical references (page 11).
517 3 $aStatic internal performance of single -expansion-ramp nozzles with thrust-vectoring capability up to 60 degrees
606   $aAxisymmetric bodies$2nasat
606   $aNozzle thrust coefficients$2nasat
606   $aStatic tests$2nasat
606   $aThrust vector control$2nasat
606   $aTransonic wind tunnels$2nasat
606   $aTwo dimensional flow$2nasat
615  7$aAxisymmetric bodies.
615  7$aNozzle thrust coefficients.
615  7$aStatic tests.
615  7$aThrust vector control.
615  7$aTransonic wind tunnels.
615  7$aTwo dimensional flow.
700   $aBerrier$b Bobby L.$01389747
702   $aLeavitt$b Laurence D.
712 02$aLangley Research Center.
712 02$aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Branch,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910707970903321
996   $aStatic internal performance of single -expansion-ramp nozzles with thrust-vectoring capability up to 60$93514191
997   $aUNINA