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 highspeed 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