Some aspects of the relationship between the geometry of circular nozzles and the thermodynamic characteristics of a flow
Abstract
Computations are presented for the thermodynamic characteristics (pressure, velocity, density, temperature) of an isentropic, subsonic gas flow through a nozzle, in order to determine the nozzle geometry. The pressure gradient along the nozzle, useful for boundary layer determination, is calculated on a high-speed computer and a method for the nozzle geometry analysis is presented. Examples are given which may have applications in turbomachinery manufacture.
- Publication:
-
Studii si Cercetary de Mecanica Aplicata
- Pub Date:
- June 1985
- Bibcode:
- 1985StCMA..44..239C
- Keywords:
-
- Gas Flow;
- Nozzle Flow;
- Nozzle Geometry;
- Thermodynamic Properties;
- Flow Velocity;
- Fluid Pressure;
- Subsonic Flow;
- Tables (Data);
- Fluid Mechanics and Heat Transfer