Numerical Design Studies on the Roll Stability of a Multi-Delta-Wing Configuration
Author:
Affiliation:
1. DLR, German Aerospace Center, 38108 Braunschweig, Germany
2. Technical University, 38108 Braunschweig, Germany
Abstract
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C037128
Reference26 articles.
1. On the nonlinear aerodynamic and stability characteristics of a generic chine-forebody slender-wing fighter configuration
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4. Study of vortex breakdown on F-16 forebody with chine and cut back LEX
5. Feasibility study of vortex interaction control on a chine forebody/delta wing configuration at high angles of attack
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