rootbrowseIAC-17C4session 99. Hypersonic Air-breathing and Combined Cycle PropulsionPapers1. analysis on the performance of a hypersonic inward turning inlet with three combined channels2. Highly reliable life time evaluation approaches for ramjet booster stage of next reusable launch vehicle3. Development of optical diagnostics for the characterization of high-velocity combustion4. A Pre-cooled and Fuel-rich Pre-burned Mixed-flow Turbofan Cycle for Ground-to-Ma5 Engines5. Thermodynamic Analysis of Helium System Cycle for the Precooled Air-breathing Combined Engine6. Successful Flight Testing of Scramjet Engine Over Wide Range of Test Conditions7. An efficient approach for tomographic reconstruction in combustion diagnostics8. Numerical Simulation in Operation Matching Characteristics of Inlet and Compressor for Air Turbo Rocket9. Researches on Rocket-Based Combined-Cycle Inlet in Northwestern Polytechnical University10. Performance Optimization Method of Turbocharged Solid Propellant Ramjet(TSPR)11. a novel liquid rocket-ramjet combined-cycle engine enhanced by a compact internal air turborocket12. Numerical investigation on the full flowpath performance of RBCC engine13. Tomography for two-dimensional gas temperature distribution based on tunable diode laser absorption spectroscopy14. Cycle analysis and optimization of the precooled Air Turbo-Ramjet15. Performance Analysis of RBCC-Based TSTO Space Transportation Systems via Multi-Objective Design Optimisation16. Performance of High Mach Number Scramjets - Tunnel vs Flight17. Modeling Scramjet Supersonic Combustion via Eddy Dissipation Model18. TRRE Technology Development19. experimental research on behavior of a non-premixed rotating detonation engine