Search Publications
Refine Results
Filter By Subject
- Aeroshells (2)
- Angle Of Attack (5)
- Chemically Reacting Flow (2)
- Combustors (2)
- Compressible Flow (2)
- Computational Fluid Dynamics (6)
- Detached Eddy Simulation (2)
- Direct Numerical Simulation (5)
- Enthalpy (3)
- Freestream Conditions (3)
- Freestream Velocity (5)
- Fuel Injection (3)
- Hypersonic Flows (4)
- Incompressible Boundary Layer (3)
- Kinetic Energy (3)
- Navier Stokes Equations (3)
- Reynolds Averaged Navier Stokes (7)
- Surface Roughness (3)
- Turbulence Models (4)
- Vortices (3)
Filter By Type
Filter By IsPartOf
- A Novel Simulation Approach for the AEDC Hypervelocity Tunnel 9 Mach 14 Nozzle
- Implementation of a Newton Method for the Rapid Propagation of Thermochemical Model Uncertainty in Hypersonic Flows
- Validation of Fluid-Structure Interaction Capabilities in US3D.
- DNS of transition to turbulence in a hypersonic boundary layer
- An Investigation into a Non-Axisymmetric Tension Shell Decelerator Concept via a Computational Design Procedure
- Numerical Simulation of Hypersonic Base Flow
- Direct Numerical Simulation of Transient Growth on a Flat Plate at Mach 3
- Hybrid RANS/LES Simulation of Injection and Mixing in the CUBRC Combustion Duct
-
Simulations of Mixing for Normal and Low-Angled Injection into a Supersonic Crossflow
December 01, 2011
- Energy Bin based Coupling Model for High Enthalpy Flows Using Prior Recombination Distribution
- Simulation of Plasma-Spark-Enhanced Mixing in Jet in Supersonic Crossflow
- Hypersonic Transition to Turbulence Triggered by Isolated Roughness Elements
- Numerical Simulations of Transition Experiments in the Hypersonic Ballistic Range
- A Nonlinear Sensitivity Solver for Aerodynamic Shape Optimization and Rapid Design Space Exploration
- Hypersonic Three-Dimensional Boundary Layer Transition on a Cone at Angle of Attack
- Hybrid Reynolds-Averaged and Large-Eddy Simulation of Scramjet Fuel Injection
- Implementation and Comparisons of Parallel Implicit Solvers for Hypersonic Flow Computations on Unstructured Meshes
- Roughness-Induced Instabilities at Mach 6: A Combined Numerical and Experimental Study
- Evaluation of Hypervelocity Carbon Dioxide Blunt Body Experiments in an Expansion Tube Facility