A Study of the Leading Edge Vortex and Tip Vortex on Prop-Fan Blades

[+] Author and Article Information
C. M. Vaczy

Hamilton Standard, Division of United Technologies Corporation, Windsor Locks, CT

D. C. McCormick

United Technologies Research Center, East Hartford, CT

J. Turbomach 109(3), 325-331 (Jul 01, 1987) (7 pages) doi:10.1115/1.3262109 History: Received February 19, 1987; Online November 09, 2009


An oil flow visualization study was conducted on the blades of a counterrotating prop-fan model, the CRP-X1. A kink in the oil streaks was interpreted as an indication of the leading edge vortex reattachment line. The leading edge vortex was found to be on the lower surface for cases with negative leading edge loading and on the upper surface for cases with positive leading edge loading. For most cases, the leading edge vortex merged with a tip vortex. The results presented here represent the first systematic study of this phenomenon.

Copyright © 1987 by ASME
Your Session has timed out. Please sign back in to continue.





Some tools below are only available to our subscribers or users with an online account.

Related Content

Customize your page view by dragging and repositioning the boxes below.

Related Journal Articles
Related eBook Content
Topic Collections

Sorry! You do not have access to this content. For assistance or to subscribe, please contact us:

  • TELEPHONE: 1-800-843-2763 (Toll-free in the USA)
  • EMAIL: asmedigitalcollection@asme.org
Sign In