Microramp Control of Supersonic Oblique Shock-Wave/Boundary-Layer Interactions
Author:
Affiliation:
1. Cambridge University, Cambridge, England CB2 1PZ, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.38022
Reference8 articles.
1. Intake Aerodynamics, Second Edition
2. INTRODUCTION TO SHOCK-INDUCED SEPARATION AND ITS PREVENTION BY DESIGN AND BOUNDARY LAYER CONTROL
3. Shock/boundary-layer interaction control with vortex generators and passive cavity
4. Effect of Microvortex Generators On Seperated Normal Shock/ Boundary Layer Interactions
5. Review of research on low-profile vortex generators to control boundary-layer separation
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