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- Effects of Variable Wall Temperature Distributions on 3D Boundary Layers
- Wall-Modeled Large Eddy Simulation of Supersonic Combustion using Flamelet/Progress-Variable Modeling
- Computations of High Enthalpy Shock-waves in Electric Arc Shock-Tube (EAST) at NASA Ames
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Characterization of Freestream Disturbances in Conventional Hypersonic Wind Tunnels
March 01, 2019
Although low-disturbance (“quiet”) hypersonic wind tunnels are believed to provide more reliable extrapolation of boundary-layer transition behavior from ground to flight, the presently available quiet facilities are limited to Mach 6, moderate Reynolds ... - Numerical Study of Trip Spacing in Hypersonic Boundary Layer Transition
- Effects of Freestream Reynolds Number and Trip Height on High-Speed Transition
- An Improved Ducros Sensor for the Simulation of Compressible Flows with Shocks
- Direct Numerical Simulation of Mach 6 Flow over a Cone with a Highly Swept Fin
- LES of the Volvo Combustion Experiment with an Ignition-Delay Variable
- Computational Study of Flow on a Sliced Cone-Flap Geometry
- Instabilities in Mach 6 Flow over a Cone with a Swept Fin
- Direct numerical simulation of BOLT hypersonic flight vehicle
- Transient growth in oblique shock wave/laminar boundary layer interactions at Mach 5.92
- Slip effects in near continuum hypersonic flow over canonical geometries
- Understanding effects of nose-cone bluntness on hypersonic boundary layer transition using input-output analysis
- Sensitivity of hypersonic flows to distributed surface roughness using input-output analysis
- Input-Output Analysis of Shock Boundary Layer Interaction
- Implementation of a Nitrogen Chemical Kinetics Model Based on ab-Initio Data for Hypersonic CFD
- Characterization of Freestream Disturbances in Conventional Hypersonic Wind Tunnels