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Evaluation of CFD for Simulation of High-Supersonic Control Surface EffectivenessThis 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.
Document ID
20210017924
Acquisition Source
Ames Research Center
Document Type
Presentation
Authors
Jim Ross (Ames Research Center Mountain View, California, United States)
Marie Denison (Ames Research Center Mountain View, California, United States)
Robert Childs (Science and Technology Corporation (United States) Hampton, Virginia, United States)
Joseph Garcia
Paul Stremel (Science and Technology Corporation (United States) Hampton, Virginia, United States)
Veronica Hawke
Hannah Spooner (Ames Research Center Mountain View, California, United States)
M. Alec Reed
Bil Kleb (Langley Research Center Hampton, Virginia, United States)
A. Neal Watkins
Paul Danehy (Langley Research Center Hampton, Virginia, United States)
Ross Burns (National Institute of Aerospace Hampton, Virginia, United States)
Timothy Fahringer (Langley Research Center Hampton, Virginia, United States)
Stephen Borg (Langley Research Center Hampton, Virginia, United States)
Philip Robinson (Johnson Space Center Houston, Texas, United States)
Date Acquired
June 24, 2021
Subject Category
Aerodynamics
Meeting Information
Meeting: AIAA Aviation Forum
Location: Virtual
Country: US
Start Date: August 2, 2021
End Date: August 6, 2021
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 951888.06.01.01
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Peer Committee
Keywords
wind tunnel

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