Correlating Surface Heat Transfer Rates and Off-Body Spectral Measurements in Roughness Dominated Hypersonic Boundary Layer Transition
Author:
Affiliation:
1. The University of Tennessee Space Institute
2. Texas A&M University
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2024-0938
Reference26 articles.
1. Hypersonic viscous flow over a slender cone. III - Laminar instability and transition
2. Observations on the Transition Process of Two-Dimensional Supersonic Wakes
3. Robust, automated processing of IR thermography for quantitative boundary-layer transition measurements
4. HIFiRE-5 Boundary-Layer Transition Measured in a Mach-6 Quiet Tunnel with Infrared Thermography
5. Preflight Ground Test Analyses of the Boundary Layer Transition (BOLT) Flight Geometry
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