Scramjet propulsion [[electronic resource] /] / edited by E.T. Curran, S.N.B. Murthy

• Record Nr.: UNINA9910457546903321
• Pubbl/distr/stampa: Reston, Va., : American Institute of Aeronautics and Astronautics, c2000
• ISBN: 1-60086-660-3; 1-60086-441-4
• Descrizione fisica: 1 online resource (1324 p.)
• Collana: Progress in astronautics and aeronautics ; ; v. 189
• Altri autori (Persone): CurranE. T; MurthyS. N. B
• Disciplina: 629.1 s; 629.134/3535
• Soggetti: Airplanes - Scramjet engines; Jet propulsion; Electronic books.
• Lingua di pubblicazione: Inglese
• Formato: Materiale a stampa
• Livello bibliografico: Monografia
• Note generali: Description based upon print version of record.
• Nota di bibliografia: Includes bibliographical references.
• Nota di contenuto: ""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""; ""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""; ""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""; ""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""; ""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""; ""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""; ""A. Objectives for Flight Testing""