Force and Moment Analysis for the High Reynolds Number Wind Tunnel Test of the Space Launch System at Ascent Conditions
Author:
Affiliation:
1. NASA Langley Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2023-0426
Reference18 articles.
1. Space Launch System Liftoff and Transition Aerodynamic Characterization in the NASA Langley 14x22' Subsonic Wind Tunnel
2. Aerodynamic Characterization and Improved Testing Methods for the Space Launch System Liftoff and Transition Environment
3. Improved Techniques for Measuring Static Ground Wind Loads on the NASA Space Launch System Mobile Launcher 2
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1. An Overview of NASA Langley Low-Speed CFD Contributions to the Space Launch System Program;AIAA SCITECH 2023 Forum;2023-01-19
2. Overview of the High Reynolds Number Ascent Wind Tunnel Test of the Space Launch System at the National Transonic Facility;AIAA SCITECH 2023 Forum;2023-01-19
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