Experimental Identification of Bistable Flow States on the Space Launch System at Liftoff Conditions
Author:
Affiliation:
1. NASA Langley Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2022-3665
Reference18 articles.
1. "Space Launch System," Available at https://www.nasa.gov/exploration/systems/sls/index.html, Accessed: 10/15/2021.
2. On the flip-flopping phenomenon of two side-by-side circular cylinders at a high subcritical Reynolds number of 1.4 × 105
3. Experimental Study on Structure of Gas Flow in Tube Banks with Tube Axes Normal to Flow : Part 1, Karman Vortex Flow from Two Tubes at Various Spacings
4. The interaction between a pair of circular cylinders normal to a stream
5. The flip-flopping wake pattern behind two side-by-side circular cylinders: A global stability analysis
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