Hypersonic Boundary-Layer Transition with Ablation and Blowing
Author:
Affiliation:
1. Purdue University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2008-3730
Reference49 articles.
1. Laminar-Turbulent Transition on Reentry Capsules and Planetary Probes
2. Flight Data for Boundary-Layer Transition at Hypersonic and Supersonic Speeds
3. Effects of High-Speed Tunnel Noise on Laminar-Turbulent Transition
4. Hypersonic laminar–turbulent transition on circular cones and scramjet forebodies
5. Effects of Roughness on Hypersonic Boundary-Layer Transition
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1. Stabilization of hypersonic boundary layer by combining micro-blowing and a porous coating;Acta Mechanica;2023-11-28
2. Modern Approaches for Calculating Flow Parameters during a Laminar–Turbulent Transition in a Boundary Layer;High Temperature;2018-01
3. Boundary Layer Transition over Blunt Hypersonic Vehicles Including Effects of Ablation-Induced Out-Gassing;6th AIAA Theoretical Fluid Mechanics Conference;2011-06-14
4. Reacting Hypersonic Boundary Layer Stability with Blowing and Suction;47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition;2009-01-05
5. Summary of Hypersonic Boundary-Layer Transition Experiments on Blunt Bodies with Roughness;Journal of Spacecraft and Rockets;2008-11
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