Nonlinear rate and amplitude effects on a generic combat aircraft model-Reference-Cited by-同舟云学术

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Nonlinear rate and amplitude effects on a generic combat aircraft model

Published:1998-01-12 Issue: Volume: Page:
ISSN:
Container-title:36th AIAA Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Ericsson Lars¹,Beyers Martin¹

Affiliation:

1. NRC of Canada Inst. for Aerospace Research, Ottawa, Canada

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1998-409

Reference21 articles.

1. 'CooperativeProgrammeon DynamicWindTunnel Experiments for Maneuvering Aircraft, AGARD-AR-305, October 1996.

2. Vortex breakdown on slender sharp-edged wings

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2. Vortex Characteristics of Pitching Double-Delta Wings;Journal of Aircraft;1999-03

3. Universality of the moving wall effect;37th Aerospace Sciences Meeting and Exhibit;1999-01-11

4. Effect of Fuselage Geometry on Delta-Wing Vortex Breakdown;Journal of Aircraft;1998-11

5. Nonlinear unsteady aerodynamics of pitching delta wings;16th AIAA Applied Aerodynamics Conference;1998-06-15

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