Add to ORKGA free-streamline flow through a cascade of semi-infinite flat plates is taken as a simplified model of the cavitation process in a helical inducer pump. The length and thickness of the resulting cavity is determined as a function of blade geometry and cavitation parameter. Loss coefficients resulting from the cavitation are estimated and representative cavity shapes are calculated to aid in designing the leading edge shape of the blades
Knowledge of the dynamic performance of pumps is essential for the prediction of transient behavior ...
Knowledge of the dynamic performance of turbopumps is essential for the prediction of instabilities ...
The cavitation behaviour of a four-blade rocket engine turbopump inducer is simulated. A...
A free-streamline flow through a cascade of semi-infinite flat plates is taken as a simplified model...
A free-streamline flow through a cascade of semi-infinite flat plates is taken as a simplified model...
After a brief review of the fundamental aspects of cavitation relevant to the operation of high-perf...
The user of a turbo machine is mainly interested only in the overall hydrodynamic performance of the...
The user of a turbo machine is mainly interested only in the overall hydrodynamic performance of the...
The user of a turbo machine is mainly interested only in the overall hydrodynamic performance of the...
Effects of the blade number on the performance of a rocket engine turbopump inducer are investigated...
After a brief review of flow-induced instabilities in turbopumps for liquid propellant feed systems ...
Liquid rocket turbopumps commonly employ axial inducers to avoid the occurrence of cavitation in the...
Knowledge of the dynamic performance of pumps is essential for the prediction of transient behavior ...
An attachment of inducer is a powerful method to improve the cavitation performance of a turbo-pump....
It is well known that leading edge sweep has a favorable effect on the cavitation of turbomachines. ...
Knowledge of the dynamic performance of pumps is essential for the prediction of transient behavior ...
Knowledge of the dynamic performance of turbopumps is essential for the prediction of instabilities ...
The cavitation behaviour of a four-blade rocket engine turbopump inducer is simulated. A...
A free-streamline flow through a cascade of semi-infinite flat plates is taken as a simplified model...
A free-streamline flow through a cascade of semi-infinite flat plates is taken as a simplified model...
After a brief review of the fundamental aspects of cavitation relevant to the operation of high-perf...
The user of a turbo machine is mainly interested only in the overall hydrodynamic performance of the...
The user of a turbo machine is mainly interested only in the overall hydrodynamic performance of the...
The user of a turbo machine is mainly interested only in the overall hydrodynamic performance of the...
Effects of the blade number on the performance of a rocket engine turbopump inducer are investigated...
After a brief review of flow-induced instabilities in turbopumps for liquid propellant feed systems ...
Liquid rocket turbopumps commonly employ axial inducers to avoid the occurrence of cavitation in the...
Knowledge of the dynamic performance of pumps is essential for the prediction of transient behavior ...
An attachment of inducer is a powerful method to improve the cavitation performance of a turbo-pump....
It is well known that leading edge sweep has a favorable effect on the cavitation of turbomachines. ...
Knowledge of the dynamic performance of pumps is essential for the prediction of transient behavior ...
Knowledge of the dynamic performance of turbopumps is essential for the prediction of instabilities ...
The cavitation behaviour of a four-blade rocket engine turbopump inducer is simulated. A...