Streamline Geometry and Equivalent Radius over a Flat Delta Wing with Cylindrical Leading Edge at Angles of Attack.
Research and development rept.,
NAVAL SHIP RESEARCH AND DEVELOPMENT CENTER BETHESDA MD AVIATION AND SURFACE EFFECTS DEPT
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An exact method has been developed for determining the streamline geometry and equivalent radius the scale factor for the normal coordinate in a streamwise coordinate system over a flat delta wing with cylindrical leading edge at angles of attack. This method requires a knowledge of the surface inviscid pressure distribution, either theoretical or experimental. With the aid of the present method, three-dimensional hypersonic heat transfer can be simply calculated through the axisymmetric analogue. Results are presented for flat delta wings traveling at hypersonic speeds and at various angles of attack.
- Fluid Mechanics