Separation Control for Aero Engine Intakes, Part 2: High-Speed Investigations
Author:
Affiliation:
1. Universität der Bundeswehr München, D-85577 Neubiberg, Germany
2. University of Cambridge, Cambridge, England CB3 0DY, United Kingdom
3. Worcester Polytechnic Institute, Worcester, Massachusetts 01609
4. Snecma, 77550 Moissy-Cramayel, France
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.B34327
Reference8 articles.
1. Measurements of Intake Separation Hysteresis in a Model Fan and Nacelle Rig
2. Separation Control for Aeroengine Intakes, Part 1: Low-Speed Investigation of Control Strategies
3. Effects of upstream boundary layer on the unsteadiness of shock-induced separation
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