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- Aerodynamic Decelerator Systems Technology Conferences (4)
- Aerospace Sciences Meetings (26)
- AIAA AVIATION Forum (4)
- AIAA Journal (6)
- AIAA SciTech Forum (8)
- AIAA SPACE Forum (1)
- Fluid Dynamics and Co-located Conferences (24)
- Guidance, Navigation, and Control and Co-located Conferences (1)
- International Space Planes and Hypersonic Systems and Technologies Conferences (1)
- Joint Propulsion Conferences (1)
- Journal of Spacecraft and Rockets (6)
- Journal of Thermophysics and Heat Transfer (4)
- Computational Analysis of Laminar Boundary Layer Separation on a Slender Cone at Angle of Attack
- High enthalpy double-wedge experiments
- Detached Eddy Simulation of the Reentry-F Flight Experiment
- Oblique Wave Disturbance Analysis of Supersonic Flow Past Axisymmetric and 2D Bodies at Angles of Attack
- Analysis of Laminar-Turbulent Transition in Hypersonic Flight Using PSE-Chem
- Transition Analysis for the HIFiRE-5 Vehicle
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Detached-Eddy Simulation of the Reentry-F Flight Experiment
July 01, 2012
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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 ... - Direct Numerical Simulation of Crossflow Instability Excited by Microscale Roughness on HIFiRE-5
- Hypersonic flow past 3-D configurations
- Simulation of Drogue Parachute for the Multi-Purpose Crew Vehicle using Computational Fluid Dynamics
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Boundary-Layer Stability Calculations for the HIFiRE-1 Transition Experiment
November 01, 2008
- An Investigation into a Non-Axisymmetric Tension Shell Decelerator Concept via a Computational Design Procedure
- Validation of Fluid-Structure Interaction Capabilities in US3D.
- Grid Sensitivity of Detached Eddy Simulation of a Mach 16 Re-Entry Configuration
- Geometric Effects on the Amplification of First Mode Instability Waves
- Numerical Simulation of Regular Surface Patterns on Sublimating Ablative Materials
- Effect of internal energy excitation on supersonic blunt-body drag
- Direct Numerical Simulation of Trip Induced Transition
- Direct boundary value solution of wave rotor flow fields