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Full Length Papers(Scramjet)(2015)
2015・Mixing flow characteristics for a transverse sonic jet injecting into a supersonic crossflow.
・The Inverse Design and Performance Evaluation of Star-shaped Hypersonic Inlets
・Hybrid Reynolds-Averaged / Large Eddy Simulation of a Cavity Flameholder; Assessment of Modeling Sensitivities
・Adjoint-Based Optimization of a Hypersonic Inlet
・Numerical simulation on detonation initiation and propagation in supersonic combustible mixtures with nonuniform species
・Design and Characterization of the Michigan Hypersonic Expansion Tube Facility (MHExT)
・T6: The Oxford University Stalker Tunnel
・An improved engine analysis and optimisation tool for hypersonic combined cycle engines
・Experimental and Numerical Performance Analysis of a Self Starting, Three-Dimensional SCRamjet Intake
・Numerical Investigation of Upstream Fuel Injection through Porous Media for Scramjet Engines via Surrogate-Assisted Evolutionary Algorithms
・Axisymmetric SCRamjet Engine Design and Performance Analysis
・Viscous Effects and Truncation Effects in Axisymmetric Busemann SCRamjet Intakes
・Simulation of Laser-Induced-Plasma Ignition in a Hypersonic Crossflow
・Large Eddy Simulation of High-Speed, Premixed Ethylene Combustion
・Numerical Investigation into the Combustion Behavior of an Inlet-Fueled Thermal-Compression-Like Scramjet
・Experimental Investigation of the Starting Behavior of a Three-Dimensional Scramjet Intake
・Study on the Effect of Air Throttling on Flame Stabilization of an Ethylene Fueled Scramjet Combustor
・Experimental Investigation on the Plasma Torch Used for Scramjet Ignition Enhancement
・Modelling and Exhaust Nozzle Flow Simulations in A Scramjet
・A Study and Design Of Scramjet Engine Inlet By Using Computational Fluid Dynamics Analysis
・COMPUTATIONAL ANALYSIS DIAMOND-SHAPED STRUT INJECTOR FOR SCRAMJET COMBUSTOR AT MACH 4.3
・EXPERIMENTAL COMPARATIVE SYNTHESIS ON THE SCRAMJET POWERED WAVERIDER VEHICLE IN HEG AND F4 WITHIN THE LAPCAT II PROJECT
・Computational Analysis of Hydrogen-Fueled Scramjet Combustor Using Cavities in Tandem Flame Holder
・Experimental investigation of a three dimensional scramjet engine at hypervelocity conditions
・A Unified Performance Analysis of a Scramjet Engine
・Fuel Injection and Combustion Study for Mach 10-12 Scramjet
・Chemical non-equilibrium flow analysis of H 2 Fueled scramjet nozzle
・Numerical simulations of single and multi-staged injection of H2 in a supersonic scramjet combustor