Effect of delta planform tip sail incidence and arrangement on wing performance
Author:
Affiliation:
1. University of the Witwatersrand, Johannesburg, South Africa
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference19 articles.
1. 4Mouch, T., McLaughlin, T., and Ashworth, J. "Unsteady Flows Produced by Small Amplitude Oscillations of the Canard of an X-29 Model/1AIAA Paper 89-2229, July/Aug. 1989.
2. Unsteady flow interactions between the wake of an oscillating airfoil and a stationary trailing airfoil
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