Some Aspects of Aircraft Dynamic Loads Due to Flow Separation Meeting (65th) Held in Cesme, Turkey on 4-9 October 1987

Abstract

This paper discusses various topics associated with the study of aircraft dynamic loads due to flow separation. Topics discussed include the need for consistent definitions of buffet and buffeting, the advantages of a consistent notation for all the papers, buffeting due to wings and other components, the alleviation of buffeting, the special difficulties of flight tests and the special advantages of buffeting measurements in cryogenic wind tunnels. Keywords: Aerodynamic loads; Boundary layer separation; Wind tunnel tests.

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Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1988
Accession Number
ADA194170

Entities

People

  • D. G. Mabey

Organizations

  • AGARD

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamic Configurations
  • Aircraft Equipment
  • Aircrafts
  • Boundary Layer
  • Computational Fluid Dynamics
  • Flow Visualization
  • Fluid Dynamics
  • Measurement
  • Pressure Gradients
  • Reynolds Number
  • Strain Gages
  • Swept Wings
  • Turbulent Mixing
  • Two Dimensional
  • Wind Tunnel Models
  • Wind Tunnel Tests
  • Wind Tunnels

Fields of Study

  • Engineering

Readers

  • Academic Conference Management
  • Aviation Science / Aeronautics.
  • Fluid Mechanics and Fluid Dynamics.