Unsteady transonic flow computations for AGARD two dimensional and three dimensional aeroelastic configurations
Abstract
Numerical results on aeroelastic standard configurations are presented. The methods used for two dimensional configurations include the small perturbations approach for inviscid flow, coupling methods for unseparated flow, coupling methods for unseparated or separated, laminar or turbulent boundary layers, and a numerical solution of the Euler equations for inviscid flow. The three dimensional configurations are studied by the transonic small disturbance approach. The detailed results are given.
- Publication:
-
NASA STI/Recon Technical Report N
- Pub Date:
- December 1986
- Bibcode:
- 1986STIN...8724645A
- Keywords:
-
- Aerodynamic Configurations;
- Aeroelasticity;
- Computerized Simulation;
- Transonic Flow;
- Unsteady Flow;
- Euler Equations Of Motion;
- Laminar Flow;
- Separated Flow;
- Viscous Flow;
- Fluid Mechanics and Heat Transfer