Accession Number:

ADA343698

Title:

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

Descriptive Note:

Corporate Author:

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

Personal Author(s):

Report Date:

1998-03-01

Pagination or Media Count:

193.0

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.

Descriptors:

• *AERODYNAMIC STABILITY
• *AERODYNAMIC LOADING
• *UNSTEADY FLOW
• COMPUTERIZED SIMULATION
• FINITE ELEMENT ANALYSIS
• DYNAMIC RESPONSE
• COMPUTATIONAL FLUID DYNAMICS
• AEROELASTICITY
• BUFFETING
• FRANCE
• EULER EQUATIONS
• NAVIER STOKES EQUATIONS
• VISCOSITY
• FLUTTER

Subject Categories:

• Aerodynamics
• Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE