An attempt is made to obtain a simple, explicit and analytical expression for the discharge coefficient of conical convergent nozzles operating under varying pressure ratios. The theoretical results based on this approach have been compared with discharge coefficient of conical jet nozzles determined experimentally covering a range of pressure ratio up to 3.25. The theory predicts the correct13; trend of the variation of discharge coefficient with respect to nozzle pressure ratio and nozzle convergence angle. Satisfactory quantitative agreement with the experimental results is possible by applying suitable correction factor for the boundary layer growth which is dependent on Reynolds number.13; The effect of variation of semi-convergence an...
This paper presents the results of tests conducted to determine the effect of the constructional ele...
A parametric investigation has been conducted to determine the jet effects on the boattail drag of n...
An investigation was conducted in the 8-by-6 foot supersonic wind tunnel on the effect of exhaust-ga...
Performance characteristics of conical jet nozzles were determined in an investigation covering a ra...
An investigation was conducted to obtain nozzle performance data with relatively large-scale models ...
AbstractNumerical works have been conducted to investigate the effect of nozzle geometries on the di...
Nozzle performance data were obtained with three "method-of-characteristics" nozzles and a 150 conic...
The discharge coefficient (Cd) is a measure of how much of the pressure energy of a nozzle is conver...
grantor: University of TorontoNon-ideal flows through angled orifices occur often in engin...
Internal performance data on a short exhaust nozzle designed by the method of characteristics were o...
Different applications of a variable area convergent-divergent nozzle are found in various parts of ...
Numerous experiments were conducted to determine factors which affect the internal performance of co...
In this paper, computational fluid dynamic (CFD) analysis and experiments have been carried out to s...
A wide variety of processes make use of plain orifice nozzles. Fuel injectors for internal combustio...
Flows of incompressible, time-independent purely viscous power-law fluids through pressure nozzle wi...
This paper presents the results of tests conducted to determine the effect of the constructional ele...
A parametric investigation has been conducted to determine the jet effects on the boattail drag of n...
An investigation was conducted in the 8-by-6 foot supersonic wind tunnel on the effect of exhaust-ga...
Performance characteristics of conical jet nozzles were determined in an investigation covering a ra...
An investigation was conducted to obtain nozzle performance data with relatively large-scale models ...
AbstractNumerical works have been conducted to investigate the effect of nozzle geometries on the di...
Nozzle performance data were obtained with three "method-of-characteristics" nozzles and a 150 conic...
The discharge coefficient (Cd) is a measure of how much of the pressure energy of a nozzle is conver...
grantor: University of TorontoNon-ideal flows through angled orifices occur often in engin...
Internal performance data on a short exhaust nozzle designed by the method of characteristics were o...
Different applications of a variable area convergent-divergent nozzle are found in various parts of ...
Numerous experiments were conducted to determine factors which affect the internal performance of co...
In this paper, computational fluid dynamic (CFD) analysis and experiments have been carried out to s...
A wide variety of processes make use of plain orifice nozzles. Fuel injectors for internal combustio...
Flows of incompressible, time-independent purely viscous power-law fluids through pressure nozzle wi...
This paper presents the results of tests conducted to determine the effect of the constructional ele...
A parametric investigation has been conducted to determine the jet effects on the boattail drag of n...
An investigation was conducted in the 8-by-6 foot supersonic wind tunnel on the effect of exhaust-ga...