High Angle of Attack Aerodynamics
Abstract
The Symposium was organized because of the continuing need for design data and principles relevant to the flight of aircraft and missiles at high angles of attack and the substantial efforts devoted to vehicles capable of controlled flight in that regime. Four sessions were held on (1) Studies of Configurations of Practical Application (10 Papers); (2) Mathematical Modelling and Supporting Investigations (12 Papers); (3) Design Methods (7 Papers), and (4) Air Intakes (2 Papers). Eight additional short presentations on these subjects are also documented. A Round Table Discussion on the state-of-art and recommendations for continuing effort in high-angle-of-attack aerodynamics is also documented in the report.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jan 01, 1979
- Accession Number
- ADA067323
Entities
Organizations
- AGARD