rootbrowseIAC-13C4session 99. Hypersonic and Combined Cycle PropulsionPapers1. Combined Cycle Propulsion System?Challenge and Prospects2. Computational Investigation of effect of Converging-Diverging Nozzle (C-D Nozzle) on the Performance of Pulse Detonation Engine(PDE)- Effects on Thrust and Inlet Pressure3. Comprehensive Consideration of Gelled fuel in hypersonic ramjet propulsion4. The constant pressure time in a piston driver of free piston shock tunnel5. experimental study on rbcc with oxygen/kerosene firstly combustion6. Measurements of two-dimensional temperature distribution in combustion using diode laser absorption spectroscopy7. Influencing Factors on the Mode Transition in a Dual-Mode Scramjet Combustor8. Mixing and combustion characteristics with lobe nozzel upstream of a V-gutter in a subsonic flow9. System Design and Analysis of Hydrocarbon Scramjet with Regeneration Cooling and Expansion Cycle10. CALCULATION OF AERODYNAMIC CHARACTERISTICS OF SAME MODEL SWIVEL NOZZLES WITH MATHEMATICAL MODELING OF REAL GAS EFFECTS11. Thermodynamic limitation on boron energy realization in ramjet propulsion12. Thermal decomposition of model endothermic hydrocarbon fuels and their mixtures13. Experimental Investigation on Angled Transverse Liquid Jet in Supersonic Crossflow