Effects of Dynamic Stall on SWECS

[+] Author and Article Information
R. B. Noll

Aerospace Systems, Inc., Burlington, Mass. 01803

N. D. Ham

Massachusetts Institute of Technology, Cambridge, Mass. 02139

J. Sol. Energy Eng 104(2), 96-101 (May 01, 1982) (6 pages) doi:10.1115/1.3266292 History: Received March 04, 1982; Online November 11, 2009


A study of dynamic stall is presented in order to define its influence on the airfoil force and moment coefficients so that these effects can be included in the calculation of small wind energy conversion system (SWECS) loads and responses. A review of past work indicates that semiempirical methods are best suited to SWECS requirements. A definition of a dynamic stall theory is made for use in SWECS design, and the theory is implemented in SWECS loads and dynamic response analyses. Sample calculations are made for a representative vertical-axis machine. It is shown that loads and moments on the blades may be underestimated if dynamic stall is not considered.

Copyright © 1982 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