rootbrowseIAC-11C4session 55. Hypersonic and Combined Cycle PropulsionPapers1. Development Status of the Hypersonic Turbojet Engine for Mach 5 flight in JAXA2. Cryogenic Fuel Management on the Precooled Turbo Jet Engine3. Evaluating heat release effects in a suprsonic reacting mixing layer with density fluctuation multiresolution analysis4. Spark Ignition and Flame Propagation in a Low Pressure Ramjet Combustor with Cavity5. Operational sensitivities of an integrated aerodynamic-ramp-injector/ gas-portfire flameholder in a supersonic combustor6. An Unstructured RANS/Flamelet CFD solver for Numerical Simulation of the Supersonic Combustion in an Integrated ARI/GP Scramjet Combustor7. The study of fuel injector arrays for scramjet combustion8. DESIGN AND OPITMIZAITON OF HYDROCARBON-FUELED SCRAMJET STAR-UP SCHEME WITH EXPANSION CYCLE9. Subassembly Matching Research and System Demonstration Tests of Air Turbo Rocket10. Numerical simulation of a mach 6 airbreathing hypersonic flight test vehicle powered by triple-module scramjets11. The Role of Exergy Analysis in Scramjet Engine Performance Analysis and Optimation12. The multi-objective optimization design for two-dimensional variable scramjet engine cowl