Turbine Separation Control Using Pulsed Vortex Generator Jets
Author:
Affiliation:
1. Air Force Insitute of Technology
2. Air Force Research Laboratory, Wright-Patterson AFB, OH 44135
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/turbomachinery/article-pdf/123/2/198/5601997/198_1.pdf
Reference18 articles.
1. Sharma et al., 1998, private communication.
2. Matsunuma, T., Abe, H., Tsutsui, Y., and Murata, K., 1998, “Characteristics of an Annular Turbine Cascade at Low Reynolds Numbers,” ASME Paper No. 98-GT-518.
3. Matsunuma, T., Abe, H., and Tsutsui, Y., 1999, “Influence of Turbulence Intensity on Annular Turbine Stator Aerodynamics at Low Reynolds Num- bers,”ASME Paper No. 99-GT-151.
4. Helton, D., 1997, private communication.
5. Lin, J. C., Howard, F. G., Bushnell, D. M., and Selby, G. V., 1990, “Investigation of Several Passive and Active Methods of Turbulent Flow Separation Control,” AIAA Paper No. 90-1598.
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