Numerical Unsteady Aerodynamic and Aeroelastic Simulation (l'Aerodynamique instationnaire numerique et la simulation de l'aeroelasticite)

Abstract

Computational unsteady aerodynamics (CUA) is a critical element in the prediction of flutter stability and dynamic response of aircraft. Linear aerodynamic methods are still the most widely used, but more advanced methods are receiving increased attention. The purpose of this Workshop was to review methods in use and to give exposure to other methods which are currently available or are in the development process.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1998
Accession Number
ADA343698

Entities

Organizations

  • AGARD

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Space

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aeroelasticity
  • Aircraft Industry
  • Aircrafts
  • Boundary Layer
  • Computational Fluid Dynamics
  • Computational Science
  • Computer Programs
  • Differential Equations
  • Flow Visualization
  • Fluid Dynamics
  • Fluid Flow
  • Mathematical Models
  • Mechanical Properties
  • Three Dimensional
  • Two Dimensional
  • Viscous Flow

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Control Systems Engineering.
  • Small Business Innovation Research Program (SBIR) EDI Research and Innovation.