Hypersonic Trip Development for BOLT-II
Author:
Affiliation:
1. US Air Force Academy
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2022-0349
Reference10 articles.
1. DNS of Transition To Turbulence in a Mach 6 Boundary Layer
2. A First Course in Turbulence
3. Extension of equilibrium turbulent heat flux models to high-speed shear flows
4. Final Design of the Boundary Layer Transition (BOLT) Flight Experiment
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3. Measurement of freestream noise in a hypersonic wind tunnel;Experiments in Fluids;2024-03-13
4. Hypersonic Ground Tests of BOLT II Using Optical Diagnostics;AIAA SCITECH 2023 Forum;2023-01-19
5. Boundary Layer Turbulence Flight Experiment in Memory of Mike Holden: Vehicle Design, Instrumentation, and Ground Test Results;AIAA SCITECH 2023 Forum;2023-01-19
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