Computation of the poststall behavior of a circulation controlled airfoil

Author:

Linton Samuel W.1

Affiliation:

1. Sterling Software at NASA Ames Research Center, Moffett Field, California 94035

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Cited by 7 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Performance analysis of a horn-type rudder implementing the Coanda effect;International Journal of Naval Architecture and Ocean Engineering;2017-03

2. Minimizing Induced Drag with Blowing Variation Along the Span of a Circulation-Controlled Wing;45th AIAA Aerospace Sciences Meeting and Exhibit;2007-01-08

3. Numerical Studies on an Active Flow Circulation Controlled Flap Concept for Aeronautical Applications;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2006

4. Analysis of a jet-controlled high-lift hydrofoil with a flap;Ocean Engineering;2003-11

5. Study on the characteristics of supersonic Coanda jet;Journal of Thermal Science;1998-09

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