Plasma Control for a Maneuvering Low-Aspect-Ratio Wing at Low Reynolds Number

Author:

Rizzetta Donald P.,Visbal Miguel R.

Publisher

ASME International

Subject

Mechanical Engineering

Reference73 articles.

1. Mueller, T. J., Kellogg, J. C., Ifju, P. G., and Shkarayev, S. V. , 2007, “Introduction to the Design of Fixed-Wing Micro Air Vehicles Including Three Case Studies,”AIAA Education Series, J. A. Schetz , ed., American Institute of Aeronautics and Astronautics.

2. Winter, H. , 1936, “Flow Phenomena on Plates and Airfoils of Short Span,” NACA Technical Memorandum 798, National Advisory Committee for Aeronautics.

3. Wadlin, K. L., Ramsen, J. A., and Vaughn, V. L. , 1955, “The Hydrodnamic Characteristics of Modified Rectangular Flat Plates Having Aspect Ratios of 1.00, 0.25, and 0.125 and Operating Near a Free Water Surface,” NACA Technical Report No. 1246, National Advisory Committee for Aeronautics.

4. Experimental Investigation of Influence of Edge Shape on the Aerodynamic Characteristics of Low Aspect Ratio Wings at Low Speeds

5. Vortex-lift prediction for complex wing planforms.

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