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  • session 5
  • 5. Hypersonic and Combined Cycle Propulsion

    Papers

    1. Development Status of the Hypersonic Turbojet Engine for Mach 5 flight in JAXA

    2. Cryogenic Fuel Management on the Precooled Turbo Jet Engine

    3. Evaluating heat release effects in a suprsonic reacting mixing layer with density fluctuation multiresolution analysis

    4. Spark Ignition and Flame Propagation in a Low Pressure Ramjet Combustor with Cavity

    5. Operational sensitivities of an integrated aerodynamic-ramp-injector/ gas-portfire flameholder in a supersonic combustor

    6. An Unstructured RANS/Flamelet CFD solver for Numerical Simulation of the Supersonic Combustion in an Integrated ARI/GP Scramjet Combustor

    7. The study of fuel injector arrays for scramjet combustion

    8. DESIGN AND OPITMIZAITON OF HYDROCARBON-FUELED SCRAMJET STAR-UP SCHEME WITH EXPANSION CYCLE

    9. Subassembly Matching Research and System Demonstration Tests of Air Turbo Rocket

    10. Numerical simulation of a mach 6 airbreathing hypersonic flight test vehicle powered by triple-module scramjets

    11. The Role of Exergy Analysis in Scramjet Engine Performance Analysis and Optimation

    12. The multi-objective optimization design for two-dimensional variable scramjet engine cowl