Double-delta-wing aerodynamics for pitching motions with and without sideslip
Author:
Affiliation:
1. U.S. Air Force Wright Laboratory, Wright-Patterson Air Force Base, Ohio 45433-7531
2. University of Notre Dame, Notre Dame, Indiana 46556-5684
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.46879
Reference33 articles.
1. Vortex interaction over double delta wings at high angles of attack
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1. Vortical Structures over a Generic Tailless Chined Forebody–Delta Wing;AIAA Journal;2024-01-17
2. Investigation on lift characteristics of a double-delta wing pitching in various reduced frequencies;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2021-03-11
3. Flow Characteristics over Double Delta Wings at Low Reynolds Numbers;Journal of Aerospace Engineering;2020-07
4. Effect of leading edge shapes on 81°/45° double-delta wing at low speeds;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2017-08-10
5. High Angle of Attack Aerodynamics;Encyclopedia of Aerospace Engineering;2010-12-15
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