Postflight Receptivity and Transition Analysis of BOLT-II Side A Descent Trajectory
Author:
Affiliation:
1. University of Minnesota Twin Cities
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2024-0703
Reference29 articles.
1. Roles of Engineering Correlations in Hypersonic Entry Boundary Layer Transition Prediction
2. Effects of High-Speed Tunnel Noise on Laminar-Turbulent Transition
3. Steen, L.c. E. "Characterization and development of nozzles for a hypersonic quiet wind tunnel," Ph.D. thesis,Purdue University, Jan. 2010. URL https://docs.lib.purdue.edu/dissertations/AAI1490698.
4. Boundary Layer Transition (BOLT) Flight Experiment Overview
5. PARABOLIZED STABILITY EQUATIONS
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