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- Numerical Simulation of the AEDC Waverider at Mach 8
- Simulation of Drogue Parachute for the Multi-Purpose Crew Vehicle using Computational Fluid Dynamics
- Validation of DES for Capsule Aerodynamics using 05-CA Wind Tunnel Test Data
- High enthalpy double-wedge experiments
- Comparison of Fluid-Structure Interaction Simulations of the MSL Parachute With Wind Tunnel Tests
- Detached Eddy Simulation of the Reentry-F Flight Experiment
- Analysis of thermo-chemical nonequilibrium models for carbon dioxideflows
- Navier-Stokes predictions of hypersonic double-cone and cylinder-flare flow fields
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Direct Simulation of Hypersonic Crossflow Instability on an Elliptic Cone
June 01, 2017
Direct numerical simulation is performed on a 38.1% scale Hypersonic International Flight Research Experimentation Program Flight 5 forebody to study stationary crossflow instability. Computations use the US3D Navier–Stokes solver to simulate Mach 6 flow ... - Computation of thermo-chemical nonequilibrium Martian atmospheric entry flows
- The effect of thermo-chemical nonequilibrium on the aerodynamics of aerobraking vehicles
- High enthalpy flow simulation challenges
- Rate-Dependent Energetic Processes in Hypersonic Flows
- Next-Generation CFD for Hypersonic and Aerothermal Flows (Invited)
- Energy Bin based Coupling Model for High Enthalpy Flows Using Prior Recombination Distribution
- A Novel Simulation Approach for the AEDC Hypervelocity Tunnel 9 Mach 14 Nozzle
- Computation of double-cone experiments in high enthalpy nitrogen
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Detailed comparison of diffusive transport phenomena between CFD and DSMC on a two-dimensional cylinder
The present paper aims to analyze the effects of the diffusion transport properties and chemical kinetics on two-dimensional hypersonic flow in the near-continuum regime. We simulate a five species air mixture with different free stream conditions using ...
- A Data-Parallel Line Relaxation method for the Navier-Stokes equations
- Translation-vibration-dissociation coupling in nonequilibrium hypersonic flows
