Effect of Vortex Generators on the Aerodynamic Wing Characteristics and Body of Revolution
Abstract
The results are presented of experimental investigations of the effect of vortex generators on the aerodynamic characteristics of streamlined bodies. Qualitative results are obtained corrobating the possibility of stabilizing the intact flow over a wing at large angles of attack. The results of an experiment on the flow over bodies of revolution with vortex generators are presented. (EDC)
Document Details
- Document Type
- Technical Report
- Publication Date
- May 03, 1990
- Accession Number
- ADA222813
Entities
People
- A. M. Mkhitaryan
- S. A. Lukashuk
Organizations
- National Air and Space Intelligence Center