Effect of Pitch Rate on Near-Surface Topology on a Delta Wing
Author:
Affiliation:
1. Lehigh University, Bethlehem, Pennsylvania 18015
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J050097
Reference43 articles.
1. Unsteady aerodynamics of nonslender delta wings
2. Recent developments in delta wing aerodynamics
3. Leading-Edge Vortex Structure of Nonslender Delta Wings at Low Reynolds Number
4. An Investigation of Vortex Flows over Low Sweep Delta Wings
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3. Dynamic lift characteristics of nonslender delta wing in large-amplitude-pitching;Aerospace Science and Technology;2020-10
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