Influence of Laminar Boundary-Layer Transition on Entry Vehicle Designs
Author:
Affiliation:
1. Northrop-Grumman Corporation, San Bernardino, California 92408
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.30047
Reference30 articles.
1. Boundary layer instability, transition and control
2. Flight Data for Boundary-Layer Transition at Hypersonic and Supersonic Speeds
3. Hypersonic laminar–turbulent transition on circular cones and scramjet forebodies
4. Laminar-Turbulent Transition on Reentry Capsules and Planetary Probes
5. Review and Synthesis of Roughness-Dominated Transition Correlations for Reentry Applications
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