An Investigation of Separation Models for the Prediction of Maximum Lift.
Abstract
The research reported here has as its objective the development of a separation model which can be incorporated into existing viscous/potential flow interaction analysis. This would provide an engineering analysis tool which would be of considerable use to both rotary and fixed wing aerodynamicists. To implement this study, three separation models were considered. The different models investigated and the results to date are described. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Jun 30, 1976
- Accession Number
- ADA027359
Entities
People
- B. Maskew
- F. A. Dvorak