Dr Wilson Chan
Current affiliation: University of Queensland
Subject: Aeronautics
Primary location: Australia
Freejet Testing of the 75%-scale HIFiRE 7 REST Scramjet Engine
Published in:19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
Publication date:2014-06-13
Drag Reduction by Boundary-Layer Combustion: Effects of Flow Disturbances from Rectangular-to-Elliptical-Shape-Transition Inlets
Published in:Journal of Propulsion and Power
Publication date:2015-09-01
Drag Reduction by Boundary-Layer Combustion: Influence from Disturbances Typical of Cross-Stream Fuel-Injection
Published in:Journal of Propulsion and Power
Publication date:2015-09-01
Suitability of the k-ω turbulence model for scramjet flowfield simulations
Published in:International Journal for Numerical Methods in Fluids
Publication date:2011-10-07k-ω TURBULENCE MODEL FOR SCRAMJET FLOWFIELD SIMULATIONS
Validating the k-ω Turbulence Model for 3D Flows within the CFD Solver Eilmer
Published in:Applied Mechanics and Materials
Publication date:2016-07-01
Ignition Experiments of Hydrocarbons in a Mach 8 Shape-Transitioning Scramjet Engine
Published in:Journal of Propulsion and Power
Publication date:2016-11-01