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[null,"1.","Record Nr.",null,"UNINA9910957339403321"]
[null,null,"Titolo",null,"Scramjet propulsion / / edited by E.T. Curran, S.N.B. Murthy"]
[null,null,"Pubbl/distr/stampa",null,"Reston, Va., : American Institute of Aeronautics and Astronautics, c2000"]
[null,null,"ISBN",null,"1-60086-660-3"]
[{"$nulls":4},"1-60086-441-4"]
[null,null,"Edizione",null,"[1st ed.]"]
[null,null,"Descrizione fisica",null,"1 online resource (1324 p.)"]
[null,null,"Collana",null,"Progress in astronautics and aeronautics ; ; v. 189"]
[null,null,"Disciplina",null,"629.1 s"]
[{"$nulls":4},"629.134/3535"]
[null,null,"Soggetti",null,"Airplanes - Scramjet engines"]
[{"$nulls":4},"Jet propulsion"]
[null,null,"Lingua di pubblicazione",null,"Inglese"]
[null,null,"Formato",null,"Materiale a stampa"]
[null,null,null,"Livello bibliografico","Monografia"]
[null,null,null,"Note generali","Description based upon print version of record."]
[null,null,null,"Nota di bibliografia","Includes bibliographical references."]
[null,null,"Nota di contenuto",null,"\"\"Cover\"\"; \"\"Title\"\"; \"\"Copyright\"\"; \"\"Contents\"\"; \"\"Preface\"\"; \"\"Introduction\"\"; \"\"I. International Efforts\"\"; \"\"II. Inlets, Combustors, and Fuels\"\"; \"\"III. Overall Systems\"\"; \"\"IV. Future Developments\"\"; \"\"V. Closing Comments\"\"; \"\"References\"\"; \"\"Chapter 1 Scramjet Testing in the T3 and T4 Hypersonic Impulse Facilities\"\"; \"\"Nomenclature\"\"; \"\"I. History, Aims, and Developments\"\"; \"\"II. Facility and Instrumentation\"\"; \"\"III. Fuel-Injection Systems\"\"; \"\"A. Wall-Injection Combustion Results\"\"; \"\"B. Wall-Injection Film-Cooling Results\"\"; \"\"C. Port-Injection Results\"\"; \"\"D. Central Injection\"\""]
[{"$nulls":4},"\"\"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\"\""]
[{"$nulls":4},"\"\"Chapter 2 Scramjet Developments in France\"\"\"\"I. Historical Overview\"\"; \"\"II. Basic Research on Diffusion Flame Combustion (1962â€?1967)\"\"; \"\"A. Combustion in a Cylindrical Duct\"\"; \"\"B. Freejet Test\"\"; \"\"C. Combustion in a Divergent Duct\"\"; \"\"D. Synthesis\"\"; \"\"III. ESOPE Program (1966â€?1973)\"\"; \"\"A. Origin and Principal Aims\"\"; \"\"B. Studies Results\"\"; "]
[{"$nulls":4},"\"\"C. Synthesis\"\"; \"\"IV. Studies on Shock-Induced Combustion\"\"; \"\"A. Principle\"\"; \"\"B. ENSMA and LATECAM Studies\"\"; \"\"V. Prepha Program (1992â€?1997)\"\"; \"\"A. Origin and Principal Aims\"\"; \"\"B. System Studies\"\""]
[{"$nulls":4},"\"\"C. Development of New Test Facilities\"\"\"\"D. Numerical Means\"\"; \"\"E. Development of Scramjet Components\"\"; \"\"Color Plates\"\"; \"\"F. Materials and Cooled Structures\"\"; \"\"G. Flight Testing\"\"; \"\"VI. Perspectives\"\"; \"\"A. Space Application\"\"; \"\"B. Missile Application\"\"; \"\"References\"\"; \"\"Chapter 3 Scramjet Investigations Within the German Hypersonics Technology Program (1993â€?1996)\"\"; \"\"I. German Hypersonics Technology Program and Scramjet-Related Activities\"\"; \"\"A. German Hypersonics Technology Program\"\"; \"\"B. Scramjet Related Activities Within the HTP\"\""]
[{"$nulls":4},"\"\"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\"\""]
[{"$nulls":4},"\"\"A. Objectives for Flight Testing\"\""]
[null,null,null,"Sommario/riassunto","Supersonic combustion ramjet (SCRJ) engine research and development begun some 40 years ago is the key to airbreathing hypersonic flight. Many unexpected complexities of SCRJ engine combustion and combustor-inlet interaction have been continuing challenges. However, valuable progress has been made in several aspects. In the next few years, it would appear that significant flight testing will take place in several countries and this should lead to further understanding of SCRJ processes in engine design for cruise and accelerator vehicle applications."]