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- Transition Analysis for the HIFiRE-5 Vehicle
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Evaluation of Wall Modeled Large Eddy Simulation of Cold Wall Hypersonic Boundary Layer
Large eddy simulation (LES) of wall bounded high Reynolds number flows is challenging due to strict cell size and time-step requirements necessary to resolve the inner layer. This restriction motivated the development of wall models which approximate the ...
- Detailed simulation of nitrogen dissociation in shock waves
- Hypersonic flow past 3-D configurations
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Boundary-Layer Stability Calculations for the HIFiRE-1 Transition Experiment
November 01, 2008
- Implementation of a Newton Method for the Rapid Propagation of Thermochemical Model Uncertainty in Hypersonic Flows
- Effect of Water Vapor on the AEDC Tunnel 9 Mach 14 Nozzle Flow
- Multi-spectral shocklayer radiance from a hypersonic slender body
- The computation of radiation from nonequilibrium hypersonic flows
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Advanced Model of Nitric Oxide Formation in Hypersonic Flows
April 01, 1998
- Flow Control of Swept Fin Shock Interactions by Laser-Induced Plasmas
- Detailed simulation of nitrogen dissociation over a sphere
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Detailed comparison of diffusive transport phenomena between CFD and DSMC
The present paper focuses on comparing state-of-the-art CFD and DSMC codes developed at the University of Minnesota; we compare results obtained with US3D, a code routinely used for complex hypersonic CFD simulations with those obtained using MGDS, a code ...
- An overlay method for calculating excited state species properties in hypersonic flows
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Energy Bin Model for High-Enthalpy Flows Using Prior Recombination Distribution
October 01, 2012
- Calculation of nonequilibrium two phase flows in a combustion heated hypersonic wind tunnel
- Multi-spectral shocklayer radiance from a hypersonic slender body
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Vehicle-Scale Simulations of Hypersonic Flows using the MMT Chemical Kinetics Model
The Modified Marrone-Treanor (MMT) chemical kinetics model has recently been developed for and implemented in CFD codes suitable for vehicle-scale simulation. The MMT model is based on ab-initio quantum chemistry data and it is designed for hypersonic ...
- Boundary Layer Stability Analysis of the Free-Piston Shock Tunnel HIEST Transition Experiments
- Analysis of thermo-chemical nonequilibrium models for carbon dioxideflows
