TAWFIVE: A user's guide
Abstract
The Transonic Analysis of a Wing and Fuselage with Interacted Viscous Effects (TAWFIVE) was developed. A finite volume full potential method is used to model the outer inviscid flow field. First-order viscous effects are modeled by a three dimensional integral boundary layer method. Both turbulent and laminar boundary layers are treated. Wake thickness and curvature effects are modeled using a two dimensional strip method. A very brief discussion of the engineering aspects of the program is given. The input and use of the program are covered in great detail.
- Publication:
-
NASA STI/Recon Technical Report N
- Pub Date:
- September 1983
- Bibcode:
- 1983STIN...8335317M
- Keywords:
-
- Computer Techniques;
- Three Dimensional Flow;
- Turbulent Boundary Layer;
- Viscous Flow;
- Finite Volume Method;
- Flow Velocity;
- Fuselages;
- Input/Output Routines;
- Mathematical Models;
- Transonic Speed;
- Fluid Mechanics and Heat Transfer