Evaluation of a surface panel method coupled with several boundary layer analyses
Abstract
Three boundary layer models are interacted with an inviscid panel method to evaluate their capabilities to predict aerodynamic performance characteristics. These boundary layer models include two two-dimensional boundary layer models and one three-dimensional boundary layer model. Previously reported discrepancies between the transpiration and surface displacement inviscid boundary layer simulations are discussed and resolved. Results from each of the models are compared with experimental data.
- Publication:
-
AIAA, Aerospace Sciences Meeting
- Pub Date:
- January 1983
- Bibcode:
- 1983aiaa.meetX....K
- Keywords:
-
- Computational Fluid Dynamics;
- Inviscid Flow;
- Panel Method (Fluid Dynamics);
- Three Dimensional Boundary Layer;
- Two Dimensional Boundary Layer;
- Aspect Ratio;
- Sweep Angle;
- Swept Wings;
- Three Dimensional Models;
- Two Dimensional Models;
- Viscous Flow;
- Fluid Mechanics and Heat Transfer