LEADER 03489nam 22006852 450 001 9910454516103321 005 20151005020621.0 010 $a0-511-69899-2 010 $a1-107-19546-2 010 $a9786612393075 010 $a1-282-39307-3 010 $a0-511-64702-6 010 $a0-511-59118-7 010 $a0-511-65110-4 010 $a0-511-59304-X 010 $a0-511-59211-6 010 $a0-511-62701-7 010 $a0-511-59497-6 035 $a(CKB)1000000000784266 035 $a(EBL)452025 035 $a(OCoLC)609843103 035 $a(SSID)ssj0000342684 035 $a(PQKBManifestationID)11231074 035 $a(PQKBTitleCode)TC0000342684 035 $a(PQKBWorkID)10284713 035 $a(PQKB)10610439 035 $a(UkCbUP)CR9780511627019 035 $a(MiAaPQ)EBC452025 035 $a(Au-PeEL)EBL452025 035 $a(CaPaEBR)ebr10329761 035 $a(CaONFJC)MIL239307 035 $a(OCoLC)438730818 035 $a(EXLCZ)991000000000784266 100 $a20090916d2009|||| uy| 0 101 0 $aeng 135 $aur||||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 14$aThe scramjet engine $eprocesses and characteristics /$fCorin Segal$b[electronic resource] 210 1$aCambridge :$cCambridge University Press,$d2009. 215 $a1 online resource (xvi, 253 pages) $cdigital, PDF file(s) 225 1 $aCambridge aerospace series ;$v25 300 $aTitle from publisher's bibliographic system (viewed on 05 Oct 2015). 311 $a1-107-40252-2 311 $a0-521-83815-0 320 $aIncludes bibliographical references and index. 327 $aTheoretical background -- High-temperature gas dynamics and hypersonic effects -- Cycle analyses and energy management -- Inlets and nozzles -- Supersonic combustion processes -- Testing methods and wind tunnels -- Computational fluid dynamic methods and solutions for high-speed reacting flows. 330 $aThe renewed interest in high-speed propulsion has led to increased activity in the development of the supersonic combustion ramjet engine for hypersonic flight applications. In the hypersonic regime the scramjet engine's specific thrust exceeds that of other propulsion systems. This book, written by a leading researcher, describes the processes and characteristics of the scramjet engine in a unified manner, reviewing both theoretical and experimental research. The focus is on the phenomena that dictate the thermo-aerodynamic processes encountered in the scramjet engine, including component analyses and flowpath considerations; fundamental theoretical topics related to internal flow with chemical reactions and non-equilibrium effects, high-temperature gas dynamics, and hypersonic effects are included. Cycle and component analyses are further described, followed by flowpath examination. Finally, the book reviews experimental and theoretical capabilities and describes ground testing facilities and computational fluid dynamics facilities developed for the study of time-accurate, high-temperature aerodynamics. 410 0$aCambridge aerospace series ;$v25. 606 $aAirplanes$xScramjet engines 615 0$aAirplanes$xScramjet engines. 676 $a629.134/353 700 $aSegal$b Corin$f1952-$0847003 801 0$bUkCbUP 801 1$bUkCbUP 906 $aBOOK 912 $a9910454516103321 996 $aThe scramjet engine$91892148 997 $aUNINA