INFLUENCE OF SPOILERS ON THE AERODYNAMIC CHARACTERISTICS OF A WING AND A SOLID 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 which confirm the possibility of stabilizing the intact flow around a wing at large angles of attack. The results of an experiment on the flow around bodies of revolving vortex generators are presented. Coefficient of a revolving body on the Reynolds number for various conditions of flow are given. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Aug 07, 1969
- Accession Number
- AD0699258
Entities
People
- A. M. Mkhitaryan
- S. A. Lukashuk
- V. D. Trubenok
- V. Ya. Fridland
Organizations
- National Air and Space Intelligence Center