The Interaction of Rolling Vortices With a Turbulent Boundary Layer
Author:
Affiliation:
1. Department of Engineering Science and Mechanics, Virginia Polytechnic Institute and State University, Blacksburg, VA 24061-0219
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/fluidsengineering/article-pdf/117/4/564/5684447/564_1.pdf
Reference21 articles.
1. Booth E. R. , and YuY. C., 1986, “Two-Dimensional Blade-Vortex Visualization Investigation,” AIAA Journal, Vol. 24, pp. 1468–1473.
2. Booth, E. R., 1986, “Surface Pressure Measurement During Low Speed Two-Dimensional Blade-Vortex Interaction,” AIAA Paper No. 86-1856.
3. Consigny H. , GravelleA., and MolinaroR., 1984, “Aerodynamic Characteristics of a Two-Dimensional Moving Spoiler in Subsonic and Transonic Flow,” Journal of Aircraft, Vol. 21, pp. 687–693.
4. Francis M. S. , KeeseeJ. E., LangJ. D., SparksG. W., and SissonG. E., 1979, “Aerodynamic Characteristics of an Unsteady Separated Flow,” AIAA Journal, Vol. 17, pp. 1332–1339.
5. Kida S. , TakaokaM., and HussainF., 1991, “Collision of Two Vortex Rings,” Journal of Fluid Mechanics, Vol. 230, pp. 583–646.
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