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Full Length Papers(Scramjet)(2014)

2014
EFFECT OF TURBULENCE MODELS ON SCRAMJET COMBUSTOR PERFORMANCE WITH KEROSENE FUEL
Thrust Augmentation by After-Burning in a Scramjet Nozzle
Radical recombination in a hydrocarbon-fueled scramjet nozzle
Conceptual design of independently configurable Mach 6.8 hydrogen fuelled dual mode scramjet propulsion system
Numerical Study of the Combustion Field in Dual-cavity Scramjet Combustor
Vortex dynamics studies in supersonic flow: Merging of co-rotating streamwise vortices
Investigations on the Influence of the In-Stream Pylon and Strut on the Performance of a Scramjet Combustor
TESTS OF THE LAPCAT II SMALL SCALE FLIGHT EXPERIMENT MODEL IN THE ONERA F4 WIND TUNNEL
Spectroscopic Measurement Techniques for Aerospace Flows
NUMERICAL MODELING OF COMPRESSIBLE FLOW AND ITS CONTROL
Application of a Real-Gas-Library Multi-Fluid-Mixing Model to Supercritical Single Injector Flow
Tailored Fuel Injection within a Mach 12 Shape Transitioning Scramjet
Equivalent Direct Connect Free-Stream Shock Tunnel Conditions for Injection Locations in an Axisymmetric Scramjet
Mixing and combustion enhancement in a Mach 12 shape-transitioning scramjet engine
Porous fuel injection with oxygen enrichment in a viable scramjet engine
An experimental investigation of an airframe integrated three-dimensional scramjet engine at a Mach 10 flight condition
CFD Simulation of Internal Flow Field of Dual-mode Scramjet
Measurements for fuel reforming for scramjet thermal management and combustion optimization: Status of the COMPARER project
Transition Prediction for Scramjet Intakes Using the gamma-Re_theta_t Model Coupled to Two Turbulence Models
Simplified procedure for controlling pressure distribution of a scramjet combustor
Exploiting Active Subspaces to Quantify Uncertainty in the Numerical Simulation of the HyShot II Scramjet
Effects of Air Vitiation on Scramjet Performance Based on Thermodynamic Cycle Analysis
Investigations on the influence of the in-stream pylon and strut on the performance of a scramjet combustor
TRANSITION MODELING FOR HYPERSONIC AIR INTAKE FLOWS IN SCRAMJET APPLICATIONS
A NUMERICAL INVESTIGATION OF SCRAMJET ENGINE AIR INTAKES FOR THE 14-X HYPERSONIC VEHICLE
Performance Analysis of Double Cavity Based Scramjet Combustion at Mach 2 using CFD
CFD Analysis of Single and Double Cavity Based Scramjet Combustion with Front Ramp Angle at Mach 2
(AIAA2014-3180)Parallelization of Unsteady Adaptive Mesh Refinement for Unstructured Navier-Stokes Solvers