Aerodynamic modeling of an oscillating wing with external stores
Author:
Affiliation:
1. USAF, Wright Aeronautical Laboratories, Wright-Patterson AFB, Ohio
2. Boeing Aerospace Co., Seattle, Wash.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1981-648
Reference20 articles.
1. Advanced panel-type influence coefficient methods applied to subsonic flows
2. Ehlers, E.F., Epton, M.A., Johnson, F.T., Magnus, A.E., and Rubbert, P.E. "A Higher Order Panel Method for Linearized Supersonic, NASA CR-3062, 1979.
3. Advanced panel-type influence coefficient methods applied to unsteady three dimensional potential flows
4. Analysis and design of wing-body combinations at subsonic and supersonic speeds.
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1. Unsteady supersonic computations of arbitrary wing-body configurations including external stores;Journal of Aircraft;1990-02
2. Transonic aeroelasticity of wings with tip stores;Journal of Aircraft;1987-10
3. Unsteady transonics of a wing with tip store;Journal of Aircraft;1986-08
4. Unsteady transonics of a wing with tip store;24th Aerospace Sciences Meeting;1986-01-06
5. An algorithm for unsteady transonic flow about tapered wings;17th Fluid Dynamics, Plasma Dynamics, and Lasers Conference;1984-06-25
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