Aircraft Dynamic Loads due to Flow Separation (Les Contraintes Aerodynamiques Imposees aux Aeronefs par le Decollement de l'Ecoulement)
Abstract
This meeting was intended to provided state-of-the-art review of all types of separated-flow dynamic problems to be encountered in present and future aircraft. In particular, the Meeting concentrated on the following topics: (1) Evaluation of aerodynamic buffet input characteristics; (2) In-flight and wind tunnel buffeting measurements; and (3) Aeroelastic buffeting prediction techniques.
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 01, 1990
- Accession Number
- ADA229916
Entities
Organizations
- AGARD