Large-time boundary-layer computations at a rear stagnation point using the asymptotic structure
Abstract
A procedure is proposed for large-time boundary-layer computations at a rear stagnation point where the double structure is implemented in a relatively straightforward manner by using the Keller Cebeci box method (1971). Results are compared with those of Howarth and Robbins (1972).
- Publication:
-
Symposium on Numerical and Physical Aspects of Aerodynamic Flows
- Pub Date:
- 1981
- Bibcode:
- 1981snpa.procS....W
- Keywords:
-
- Boundary Layer Equations;
- Laminar Boundary Layer;
- Stagnation Point;
- Trailing Edges;
- Asymptotic Methods;
- Grids;
- Skin Friction;
- Transformations (Mathematics);
- Velocity Distribution;
- Fluid Mechanics and Heat Transfer