Control of Unsteady Aerodynamic Forces
Abstract
The aerodynamic properties of an airfoil under unsteady conditions are very different from ones in steady conditions because the vortex generated by unsteady separation greatly modifies the loading on the wing. In this study, a fundamental approach was taken to investigate the lift and the velocity field of unsteady airfoils. Keywords: Airfoil unsteady water channels, Delta wings, Lift, Flow visualization.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jul 25, 1990
- Accession Number
- ADA227365
Entities
People
- Chiang Shih
- Chih-ming Ho
- Hank Lin
- Ismet Gursul
- Mario Lee
Organizations
- University of Southern California