Effect of Wall Cooling on the Stability of a Hypersonic Boundary Layer over a Slender Cone
Author:
Affiliation:
1. University of Maryland, College Park
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2021-2866
Reference24 articles.
1. Transition Analysis for the Ascent Phase of HIFiRE-1 Flight Experiment
2. HIFiRE-1 Ascent-Phase Boundary-Layer Transition
3. The Hythirm Project: Flight Thermography of the Space Shuttle During Hypersonic Re-Entry
4. Hypersonic Navier Stokes Comparisons to Orbiter Flight Data
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1. Controlling hypersonic boundary layer transition with localized cooling and metasurface treatments;Scientific Reports;2024-07-10
2. Hypersonic Boundary-Layer Disturbances on a Cooled, Slender Cone at Mach 6;Journal of Spacecraft and Rockets;2023-03
3. Local Wall Cooling Effects on Hypersonic Boundary-Layer Stability;Journal of Spacecraft and Rockets;2023-03
4. Numerical investigation of the effects of wall heating and cooling on the nonlinear transition stages for a sharp cone at Mach 6;AIAA SCITECH 2022 Forum;2022-01-03
5. Boundary-Layer Disturbances and Surface Heat-Flux Profiles on a Cooled Slender Cone;AIAA SCITECH 2022 Forum;2022-01-03
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