LEADER 04774nam 2200637 a 450 001 9910781422703321 005 20230422050643.0 010 $a1-60086-660-3 010 $a1-60086-441-4 035 $a(CKB)2550000000072871 035 $a(EBL)3111567 035 $a(SSID)ssj0000565876 035 $a(PQKBManifestationID)12198631 035 $a(PQKBTitleCode)TC0000565876 035 $a(PQKBWorkID)10533196 035 $a(PQKB)11659467 035 $a(Au-PeEL)EBL3111567 035 $a(CaPaEBR)ebr10516671 035 $a(OCoLC)774285718 035 $a(MiAaPQ)EBC3111567 035 $a(EXLCZ)992550000000072871 100 $a20020304d2000 uy 0 101 0 $aeng 135 $aur|n|---||||| 181 $ctxt 182 $cc 183 $acr 200 00$aScramjet propulsion$b[electronic resource] /$fedited by E.T. Curran, S.N.B. Murthy 210 $aReston, Va. $cAmerican Institute of Aeronautics and Astronautics$dc2000 215 $a1 online resource (1324 p.) 225 1 $aProgress in astronautics and aeronautics ;$vv. 189 300 $aDescription based upon print version of record. 311 $a1-56347-322-4 320 $aIncludes bibliographical references. 327 $a""Cover""; ""Title""; ""Copyright""; ""Contents""; ""Preface""; ""Introduction""; ""I. International Efforts""; ""II. Inlets, Combustors, and Fuels""; ""III. Overall Systems""; ""IV. Future Developments""; ""V. Closing Comments""; ""References""; ""Chapter 1 Scramjet Testing in the T3 and T4 Hypersonic Impulse Facilities""; ""Nomenclature""; ""I. History, Aims, and Developments""; ""II. Facility and Instrumentation""; ""III. Fuel-Injection Systems""; ""A. Wall-Injection Combustion Results""; ""B. Wall-Injection Film-Cooling Results""; ""C. Port-Injection Results""; ""D. Central Injection"" 327 $a""IV. Combustion/Mixing Processes""""A. Mixing Controlled Combustion""; ""B. Kinetically Controlled Combustion""; ""C. Shock-Induced Ignition""; ""D. Shock-Induced Mixing""; ""V. Simple Theoretical Combustor and Thrust Model""; ""VI. Experimental Results of Specific Impulse""; ""VII. Effects of Atomic Oxygen and Nitric Oxide in the Freestream""; ""VIII. Different Fuels""; ""A. Hydrocarbon Fuels""; ""B. Silane-Enriched Fuels""; ""IX. Integrated Scramjet Measurements""; ""X. Skin-Friction Measurements""; ""XI. Discussion and Review""; ""Acknowledgments""; ""Bibliography"" 327 $a""Chapter 2 Scramjet Developments in France""""I. Historical Overview""; ""II. Basic Research on Diffusion Flame Combustion (1962a???1967)""; ""A. Combustion in a Cylindrical Duct""; ""B. Freejet Test""; ""C. Combustion in a Divergent Duct""; ""D. Synthesis""; ""III. ESOPE Program (1966a???1973)""; ""A. Origin and Principal Aims""; ""B. Studies Results""; ""C. Synthesis""; ""IV. Studies on Shock-Induced Combustion""; ""A. Principle""; ""B. ENSMA and LATECAM Studies""; ""V. Prepha Program (1992a???1997)""; ""A. Origin and Principal Aims""; ""B. System Studies"" 327 $a""C. Development of New Test Facilities""""D. Numerical Means""; ""E. Development of Scramjet Components""; ""Color Plates""; ""F. Materials and Cooled Structures""; ""G. Flight Testing""; ""VI. Perspectives""; ""A. Space Application""; ""B. Missile Application""; ""References""; ""Chapter 3 Scramjet Investigations Within the German Hypersonics Technology Program (1993a???1996)""; ""I. German Hypersonics Technology Program and Scramjet-Related Activities""; ""A. German Hypersonics Technology Program""; ""B. Scramjet Related Activities Within the HTP"" 327 $a""II. Theoretical Investigations for Scramjet Intake Designs""""A. Activities at Dasa-MT633""; ""B. Activities at RWTH Aachen""; ""III. Theoretical and Experimental Investigations of Scramjet Combustion at TsAGI and DLR Lampoldshausen""; ""A. Combustor Model Design""; ""B. Fuel-Injection Modules""; ""C. Test Results""; ""IV. Freejet Wind-tunnel Testing of Scramjet Propulsion Systems at TsAGI""; ""A. Scramjet Propulsion System Model Concept""; ""B. Testing Focus""; ""C. Test Results""; ""V. Considerations for Flight Testing Small-Scale Scramjet Modules Using the RADUGA-D2 Flying Testbed"" 327 $a""A. Objectives for Flight Testing"" 410 0$aProgress in astronautics and aeronautics ;$vv. 189. 606 $aAirplanes$xScramjet engines 606 $aJet propulsion 615 0$aAirplanes$xScramjet engines. 615 0$aJet propulsion. 676 $a629.1 s 676 $a629.134/3535 701 $aCurran$b E. T$01463131 701 $aMurthy$b S. N. B$013320 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bMiAaPQ 906 $aBOOK 912 $a9910781422703321 996 $aScramjet propulsion$93779408 997 $aUNINA