All Stories

  1. Aerodynamic Design of Nozzles with Uniform Outflow for Hypervelocity Ground-Test Facilities
  2. Freejet Testing of the HIFiRE 7 Scramjet Flowpath at Mach 7.5
  3. Ignition Experiments of Hydrocarbons in a Mach 8 Shape-Transitioning Scramjet Engine
  4. Validating the k-ω Turbulence Model for 3D Flows within the CFD Solver Eilmer
  5. Drag Reduction by Boundary-Layer Combustion: Effects of Flow Disturbances from Rectangular-to-Elliptical-Shape-Transition Inlets
  6. Drag Reduction by Boundary-Layer Combustion: Influence from Disturbances Typical of Cross-Stream Fuel-Injection
  7. Freejet Testing of the 75%-scale HIFiRE 7 REST Scramjet Engine
  8. Suitability of the k-ω turbulence model for scramjet flowfield simulations