AGARD Three-Dimensional Aeroelastic Configurations

Abstract

The aeroelastician needs reliable and efficient methods for the calculation of unsteady aerodynamic forces in the frequently critical transonic speed regime. The development of such methods may be enhanced by the availability of a limited number of test cases for the comparison of competing methods. This report contains such test cases for five clean, isolated wings. Wing geometric descriptions, airfoil coordinates, and suggested aerodynamic conditions for each are included.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1982
Accession Number
ADA115045

Entities

People

  • Samuel R. Bland

Organizations

  • AGARD

Tags

Communities of Interest

  • Space

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Air Force
  • Aspect Ratio
  • Computational Science
  • Control Surfaces
  • Fluid Dynamics
  • Geometry
  • Leading Edges
  • Mach Number
  • Nato
  • Pressure Distribution
  • Reynolds Number
  • Standards
  • Three Dimensional
  • Two Dimensional
  • United States
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Aerodynamics/Aeronautics.
  • Computational Modeling and Simulation