Free jet expansion in a rapidly rotating gas
Abstract
The Newtonian thin shock layer approximation is applied in calculating the inviscid structure of a free jet exhausting into a rotating gas. Attention is given to the equations for jet boundary and barrel shock shape. The Runge-Kutta-Gill method is used to determine jet boundary shapes when employing numerical integration of thin shock layer assumptions.
- Publication:
-
AIAA Journal
- Pub Date:
- April 1980
- DOI:
- Bibcode:
- 1980AIAAJ..18..471M
- Keywords:
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- Flow Geometry;
- Free Jets;
- Gas Flow;
- Jet Exhaust;
- Rotating Fluids;
- Approximation;
- Flow Distribution;
- Flow Equations;
- Shock Layers;
- Velocity Distribution;
- Fluid Mechanics and Heat Transfer