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- Orbiter Boundary Layer Stability Analysis at Flight Entry Conditions
- Hypersonic Navier Stokes Comparisons to Orbiter Flight Data
- Supersonic Combustor Fuel Injection Simulations Using a Hybrid RANS/LES Approach
- Boundary Layer Stability Analysis of the Free-Piston Shock Tunnel HIEST Transition Experiments
- Analysis of Chemistry-Vibration Coupling in Diatomics for High Enthalpy Nozzle Flows
- CFD Analysis of CUBRC Base Flow Experiments
- The Potential Role of Electronically-Excited States in Recombining Flows
- Three-Dimensional Hypersonic Boundary Layer Stability Analysis with STABL-3D
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Hybrid Reynolds-Averaged and Large-Eddy Simulation of Normal Injection into a Supersonic Crossflow
May 01, 2010
- Simulations of High-Speed Flow Over an Isolated Roughness
- Simulation of Boundary Layer Transition on Elliptic Cones in Hypersonic Flow
- Hybrid RANS/LES Simulation of Transverse Jet in Supersonic Crossflow with Laser Energy Deposition
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Vibrational Modeling of CO2 in High-Enthalpy Nozzle Flows
January 01, 2010
- Numerical Simulations of Roughness Induced Instability in the Purdue Mach 6 Wind Tunnel
- Carbon Dioxide Injection for Hypervelocity Boundary Layer Stability
- Infrared Measurements of Boundary-Layer transition on an Inclined Cone at Mach 6
- Flow Simulation of Tension Cone Inflatable Aeroshell with Fluid Structure Interactions