Performance augmentation of a 60-degree delta aircraft configurationby spanwise blowing
Author:
Affiliation:
1. Technion—Israel Institute of Technology, Haifa, Israel
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.45384
Reference14 articles.
1. Possible Types of Flow at Swept Leading Edges
2. Predictions of vortex-lift characteristics by a leading-edge suctionanalogy
3. Numerical calculation of nonlinear aerodynamics of wing-body configurations
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