AGARD Two-Dimensional Aeroelastic Configurations

Abstract

The aeroelastician needs reliable efficient methods for the calculation of unsteady aerodynamic forces in the frequency critical transonic speed regime. The development of such methods can be enhanced by the availability of a limited number of test cases for the comparison of competing methods. This report contains such test cases. Geometric descriptions of seven, two-dimensional airfoils and suggested aerodynamic conditions for each are included.

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Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1979
Accession Number
ADA075104

Entities

People

  • S. R. Bland

Organizations

  • AGARD

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamic Forces
  • Aircrafts
  • Availability
  • Flow
  • Geometry
  • Materials
  • Mathematics
  • Nato
  • Republic
  • Standards
  • Three Dimensional
  • Two Dimensional
  • Two Dimensional Flow
  • United States
  • Unsteady Flow
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Life Cycle Cost Analysis