Leading-Edge Vortex Interactions at a Generic Multiple Swept-Wing Aircraft Configuration
Author:
Affiliation:
1. Technical University of Munich, 85748 Garching, Germany
Funder
Deutsche Forschungsgemeinschaft
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference26 articles.
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2. GreerH. D. “Summary of Directional Divergence Characteristics of Several High-Performance Aircraft Configurations,” NASA TN-D-6993, Nov. 1972.
3. Use of hinged strakes for lateral control at high angles of attack
4. Forebody vortex management for yaw control at high angles of attack
5. Enhanced Maneuverability of a Delta-Canard Combat Aircraft by Vortex Flow Control
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