LEADER 02434nam 2200589Ia 450 001 9910699653003321 005 20230902161736.0 035 $a(CKB)5470000002404406 035 $a(OCoLC)704909437 035 $a(EXLCZ)995470000002404406 100 $a20110303d2010 ua 0 101 0 $aeng 135 $aurmn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aComputational fluid dynamics (CFD) simulation of hypersonic turbine-based combined-cycle (TBCC) inlet mode transition$b[electronic resource] /$fJohn W. Slater and John D. Saunders ; prepared for the 16th International Space Planes and Hypersonic Systems and Technologies Conference cosponsored by the AIAA, DLR, and DGLR, Bremen, Germany, October 19-22, 2009 210 1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d[2010] 215 $a1 online resource (27 pages) $cillustrations 225 1 $aNASA/TM ;$v2010-216362 300 $aTitle from title screen (viewed on March 3, 2011). 300 $a"May 2010." 300 $a"AIAA-2009-7349." 320 $aIncludes bibliographical references (page 27) 410 0$aNASA technical memorandum ;$v216362. 517 $aComputational fluid dynamics 606 $aComputational fluid dynamics 241$2nasat 606 $aData simulation$2nasat 606 $aHypersonics$2nasat 606 $aStatic pressure$2nasat 606 $aSupersonic combustion ramjet engines$2nasat 606 $aWind tunnel tests$2nasat 606 $aAerodynamics$2nasat 606 $aBoundary layers$2nasat 615 7$aComputational fluid dynamics 241. 615 7$aData simulation. 615 7$aHypersonics. 615 7$aStatic pressure. 615 7$aSupersonic combustion ramjet engines. 615 7$aWind tunnel tests. 615 7$aAerodynamics. 615 7$aBoundary layers. 700 $aSlater$b John W$017883 701 $aSaunders$b John D$01417796 712 02$aNASA Glenn Research Center. 712 12$aAIAA/CIRA International Space Planes and Hypersonic Systems and Technologies Conference$d(16th :$f2009 :$eBremen, Germany) 801 0$bGPO 801 1$bGPO 906 $aBOOK 912 $a9910699653003321 996 $aComputational fluid dynamics (CFD) simulation of hypersonic turbine-based combined-cycle (TBCC) inlet mode transition$93527372 997 $aUNINA