Direct numerical simulation of BOLT hypersonic flight vehicle
Author:
Affiliation:
1. University of Minnesota, Twin Cities
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-2894
Reference29 articles.
1. Stability Analysis for HIFiRE Experiments
2. Ground Test Measurements of Boundary-Layer Instabilities and Transition for HIFiRE-5 at Flight-Relevant Attitudes
3. Effects of High-Speed Tunnel Noise on Laminar-Turbulent Transition
4. Mean flow and noise measurements in a Mach 3.5 pilot quiet tunnel
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