CFD Analysis of Space Launch System Solid Rocket Booster Separation within the Langley Unitary Plan Wind Tunnel
Author:
Affiliation:
1. NASA Ames Research Center
2. NASA Langley Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2021-2966
Reference42 articles.
1. Best Practices for Aero-Database CFD Simulations of Ares V Ascent
2. Best Practices for CFD Simulations of Launch Vehicle Ascent with Plumes - OVERFLOW Perspective
3. Aerodynamic Database Generation for SRB Separation from a Heavy Lift Launch Vehicle
4. CFD Simulations of the Space Launch System Ascent Aerodynamics and Booster Separation
5. Inviscid and Viscous CFD Analysis of Booster Separation for the Space Launch System Vehicle
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1. Exhaust Gas and Plume Modeling Effects for Space Launch System Abort Scenarios;Journal of Spacecraft and Rockets;2024-07
2. Launch Vehicle Ascent Computational Fluid Dynamics for the Space Launch System;Journal of Spacecraft and Rockets;2023-12-29
3. Evaluation of CFD Predictions of Cobra-MRV Control Surface Effectiveness at the NASA Langley Unitary Plan Wind Tunnel;AIAA AVIATION 2021 FORUM;2021-07-28
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