LEADER 02666oam 2200649 450 001 9910702682503321 005 20140922113430.0 035 $a(CKB)5470000002429361 035 $a(OCoLC)761221787 035 $a(EXLCZ)995470000002429361 100 $a20111115j198001 ua 0 101 0 $aeng 135 $aurmn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aDynamic response of a Mach 2.5 axisymmetric inlet and turbojet engine with a poppet-valve-controlled inlet-stability bypass system when subjected to internal and external airflow transients /$fBobby W. Sanders 210 1$aWashington, D.C. :$cNational Aeronautics and Space Administration, Scientific and Technical Information Office,$dJanuary 1980. 215 $a1 online resource (iii, 98 pages) $cillustrations 225 1 $aNASA technical paper ;$v1531 300 $aTitle from title screen (viewed Sept. 22, 2014). 300 $a"January 1980." 300 $a"Performing organization, Lewis Research Center"--Technical report documentation page. 320 $aIncludes bibliographical references (pages 27-28). 606 $aAirplanes$xTurbojet engines$xAir intakes 606 $aAirplanes$xMotors$xValves 606 $aAerodynamic stability$2nasat 606 $aBypasses$2nasat 606 $aPropulsion system performance$2nasat 606 $aSupersonic inlets$2nasat 606 $aTurbojet engines$2nasat 606 $aWind tunnel stability tests$2nasat 606 $aAirplanes$xMotors$xValves$2fast 606 $aAirplanes$xTurbojet engines$xAir intakes$2fast 615 0$aAirplanes$xTurbojet engines$xAir intakes. 615 0$aAirplanes$xMotors$xValves. 615 7$aAerodynamic stability. 615 7$aBypasses. 615 7$aPropulsion system performance. 615 7$aSupersonic inlets. 615 7$aTurbojet engines. 615 7$aWind tunnel stability tests. 615 7$aAirplanes$xMotors$xValves. 615 7$aAirplanes$xTurbojet engines$xAir intakes. 700 $aSanders$b Bobby W.$01417227 712 02$aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Office, 712 02$aLewis Research Center, 801 0$bOCLCE 801 1$bOCLCE 801 2$bOCLCQ 801 2$bOCLCF 801 2$bOCLCQ 801 2$bGPO 906 $aBOOK 912 $a9910702682503321 996 $aDynamic response of a Mach 2.5 axisymmetric inlet and turbojet engine with a poppet-valve-controlled inlet-stability bypass system when subjected to internal and external airflow transients$93524889 997 $aUNINA