Weighted residual finite element solution for internal flow field, in-depth temperature response and thermostructure
Abstract
A universal analysis technique to predict internal flow field, in-depth temperature, and thermostructure in a rocket nozzle flow field is presented. This technique is suited for computer programming and improved nozzle performance prediction is expected. Calculative and analytical results from the method are in good agreement.
- Publication:
-
Lausanne International Astronautical Federation Congress
- Pub Date:
- October 1984
- Bibcode:
- 1984laus.iafc.....J
- Keywords:
-
- Finite Element Method;
- Flow Distribution;
- Nozzle Flow;
- Rocket Nozzles;
- Temperature Distribution;
- Axial Stress;
- Boundary Value Problems;
- Flow Stability;
- Nozzle Efficiency;
- Nozzle Geometry;
- Solid Propellant Rocket Engines;
- Fluid Mechanics and Heat Transfer