Scramjet propulsion

Scramjet propulsion / edited by E.T. Curran, S.N.B. Murthy.

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Bibliographic Details
Other Authors: Curran, E. T., Murthy, S. N. B.
Format: eBook
Language:English
Published: Reston, Va. : American Institute of Aeronautics and Astronautics, ©2000.
Series:Progress in astronautics and aeronautics ; v. 189.
Subjects:
Airplanes > Scramjet engines.
Jet propulsion.
Airplanes > Scramjet engines
Jet propulsion
dissertations.
Academic theses
Academic theses.
Thèses et écrits académiques.
Online Access:Click for online access
Table of Contents:
  • 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.

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