Unsteady aerodynamics of rolling thick delta wing with high aspect ratio
Author:
Affiliation:
1. Nagoya Univ., Japan
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1998-2520
Reference12 articles.
1. Physics of vortical flows
2. Predictions of vortex-lift characteristics by a leading-edge suctionanalogy
3. High Angle of Attack Aerodynamics
4. Static and total pressure distributions around a thick delta wing with rounded leading edge
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