Accession Number:

ADA229916

Title:

Aircraft Dynamic Loads due to Flow Separation (Les Contraintes Aerodynamiques Imposees aux Aeronefs par le Decollement de l'Ecoulement)

Descriptive Note:

Corporate Author:

ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT NEUILLY-SUR-SEINE (FRANCE)

Personal Author(s):

Report Date:

1990-09-01

Pagination or Media Count:

274.0

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.

Subject Categories:

  • Aerodynamics
  • Aircraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE