Evaluation of CFD for Simulation of High-Supersonic Control-Surface Effectiveness-Reference-Cited by-同舟云学术

Evaluation of CFD for Simulation of High-Supersonic Control-Surface Effectiveness

Published:2021-07-28 Issue: Volume: Page:
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Container-title:AIAA AVIATION 2021 FORUM
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Author:

Ross James C.¹,Denison Marie¹,Childs Robert²,Garcia Joseph¹,Stremel Paul²,Hawke Veronica²,Spooner Hannah¹,Robinson Phil³,Reed Matthew⁴,Kleb William L.⁵,Watkins Neal⁵,Danehy Paul M.⁵,Burns Ross⁶,Fahringer Timothy⁵

Affiliation:

1. NASA Ames Research Center

2. Science and Technology Corporation

3. NASA Johnson Space Center

4. Jacobs

5. NASA Langley Research Center

6. National Institute of Aerospace

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2021-2964

Reference15 articles.

1. Space Launch System Booster Separation Supersonic Powered Testing with Surface and Off-body Measurements

2. Co-Optimization of Mid Lift to Drag Vehicle Concepts for Mars Atmospheric Entry

3. Cerimele, C. J., Robertson, E. A., Sostaric, R. R. (editor), Campbell, C. H., Robinson, P., Matz, D. A., Johnson, B. J., Stachowiak, S. J., Garcia, J. A., Bowles, J. V., Kinney, D. J., Theisinger, J. E. "A Rigid Mid-Lift-to-Drag Ratio Approach to Human Mars Entry, Descent, and Landing" AIAA Paper 2017-1898, Feb 2017.

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