A case for pseudo-steady aerodynamic behaviour at high motion rates
Author:
Affiliation:
1. Aiolos Engineering Corp., Toronto, Canada
2. Notre Dame, Univ., IN
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1997-617
Reference18 articles.
1. Airfoil dynamic stall at constant pitch rate and high Reynolds number
2. Low-Speed Unsteady Aerodynamics of a Pitching Straked Wing at High Incidence-Part I: Test Program
3. Future fighter technologies
4. Dynamics of air combat
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