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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