This is the set of slides describing the CFD and wind-tunnel test studying the control surfaces of the CobraMRV concept for entry, descent, and landing on Mars. Difference between the CFD and wind-tunnel results are highlighted with the intent of showing whether CFD can replace wind-tunnel testing in the high supersonic flight regime.
Evaluation of CFD for Simulation of High-Supersonic Control Surface Effectiveness
AIAA Aviation Forum ; 2021 ; Virtual, US
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Englisch