Shock-Wave/Boundary-Layer Interactions in a Model Scramjet Intake
Author:
Affiliation:
1. University of Southampton, Southampton, England SO17 1BJ, United Kingdom
2. ESA, 2200 AG Noordwijk, The Netherlands
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.41107
Reference27 articles.
1. Streamline Tracing: Technique for Designing Hypersonic Vehicles
2. Fifty Years of Shock-Wave/Boundary-Layer Interaction Research: What Next?
3. Two-dimensional numerical investigations of small-amplitude disturbances in a boundary layer at Ma=4.8: Compression corner versus impinging shock wave
4. Space and time organization in a shock-induced separated boundary layer
5. Achievements Obtained for Sustained Hypersonic Flight Within the LAPCAT Project
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