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Scramjet propulsion /
| Clasificación: | Libro Electrónico |
|---|---|
| Otros Autores: | , |
| Formato: | Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
Reston, Va. :
American Institute of Aeronautics and Astronautics,
©2000.
|
| Colección: | Progress in astronautics and aeronautics ;
v. 189. |
| Temas: | |
| Acceso en línea: | Texto completo |
Tabla de Contenidos:
- 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 (1962-1967)
- A. Combustion in a Cylindrical Duct
- B. Freejet Test
- C. Combustion in a Divergent Duct
- D. Synthesis
- III. ESOPE Program (1966-1973)
- 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 (1992-1997)
- 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 (1993-1996)
- 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
- B. RADUGA-D2 Flying Testbed
- C. Flight Test Trajectory and Integration of Scramjet in the RADUGA-D2
- References.