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Comparison of OVERFLOW Computational and Experimental Results for a Blunt Mars Entry Vehicle Concept During Supersonic Retropropulsion
Simulations of unsteady supersonic retropropulsion (SRP) flow over a Hypersonic Inflatable
Aerodynamic Decelerator (HIAD) blunt-body vehicle were performed using the OVERFLOW …
Aerodynamic Decelerator (HIAD) blunt-body vehicle were performed using the OVERFLOW …
Withdrawn: Novel Turbulence Model Tailored for Rocket Motor Exhaust Jets
R Childs - AIAA AVIATION FORUM AND ASCEND 2024, 2024 - arc.aiaa.org
This paper describes a new RANS turbulence model intended to give improved accuracy in
turbulence that is affected by compressibility, rotation and curvature, and variable density …
turbulence that is affected by compressibility, rotation and curvature, and variable density …
Comparison of OVERFLOW Computational and Experimental Results of the CobraMRV Mars Entry Vehicle Concept during Supersonic Retropropulsion
The CFD solver OVERFLOW was used to simulate the CobraMRV undergoing supersonic
retropropulsion (SRP) in the Langley Unitary Plan Wind Tunnel as part of a CFD and wind …
retropropulsion (SRP) in the Langley Unitary Plan Wind Tunnel as part of a CFD and wind …
[PDF][PDF] OVERFLOW Guidelines for Simulation of Supersonic Retropropulsion
General methods for obtaining satisfactory simulation accuracy across a range of supersonic
retropropulsive flows are recommended using comparisons between OVERFLOW …
retropropulsive flows are recommended using comparisons between OVERFLOW …
Novel Turbulence Model Tailored for Complex Rocket Motor Exhaust Jets
This paper describes a new RANS turbulence model intended to give improved accuracy in
turbulence that is affected by compressibility, rotation and curvature, and variable density …
turbulence that is affected by compressibility, rotation and curvature, and variable density …