LEADER 01868nam 2200517Ia 450 001 9910697023103321 005 20230902162024.0 035 $a(CKB)5470000002384674 035 $a(OCoLC)756767133 035 $a(EXLCZ)995470000002384674 100 $a20111012d2005 ua 0 101 0 $aeng 135 $aurcn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aDevelopment and characterization testing of an air pulsation valve for a pulse detonation engine supersonic parametric inlet test section$b[electronic resource] /$fRobert Tornabene 210 1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d[2005] 215 $a1 online resource (15 pages) $cillustrations (some color) 225 1 $aNASA/TM ;$v2005-213893 300 $aTitle from title screen (viewed on Oct. 12, 2011). 300 $a"October 2005." 410 0$aNASA technical memorandum ;$v213893. 606 $aAir flow$2nasat 606 $aCharacterization$2nasat 606 $aEngine inlets$2nasat 606 $aPulse detonation engines$2nasat 606 $aSupersonic wind tunnels$2nasat 606 $aGas valves$2nasat 606 $aWind tunnel tests$2nasat 615 7$aAir flow. 615 7$aCharacterization. 615 7$aEngine inlets. 615 7$aPulse detonation engines. 615 7$aSupersonic wind tunnels. 615 7$aGas valves. 615 7$aWind tunnel tests. 700 $aTornabene$b Robert$01410570 712 02$aNASA Glenn Research Center. 801 0$bGPO 801 1$bGPO 801 2$bGPO 906 $aBOOK 912 $a9910697023103321 996 $aDevelopment and characterization testing of an air pulsation valve for a pulse detonation engine supersonic parametric inlet test section$93499518 997 $aUNINA