ABSTRACT Two flow instabilities involving a bifurcated flow pattern were discovered for the throughflow jet in a stepped labyrinth seal. A bifurcation stability map was developed showing which combinations of tooth clearance and step height occur in which of the three flow regimes. These instabilities, along with selfsustained flow oscillations, were experimentally explored to obtain a preliminary understanding of their effect on seal leakage. Computer-captured visualization videos were used to measure the throughflow angle oscillation amplitudes, frequencies and mean flow trajectory angles. For small tooth clearances, the intermediate step height case, which exhibited the sharpest flow deflection and largest oscillation amplitude, gave the...
Unsteady flow phenomena in turbomachinery are a source of aerodynamic losses and can adversely affec...
As well known, the stability assessment of turbomachines is strongly related to internal sealing com...
Secondary flows in turbomachinery highly affect the overall efficiency and rotorstability. A prime e...
Due to the character of the original source materials and the nature of batch digitization, quality ...
Typescript (photocopy).A computational/experimental study was conducted on the incompressible flow i...
Straight-through labyrinth seal is a simple and reliable noncontact seal structure widely used in ae...
The leakage between rotational and stationary part is one of the main source of performance loss in ...
Due to the character of the original source materials and the nature of batch digitization, quality ...
3noWhen numerically simulating the performance of a complete Francis turbine, it is common practice...
The reliable prediction of the effect of various labyrinth parameters on leakage rate has not been r...
The most important issue when designing the labyrinth sealing knots is the question of the correctne...
A new type of stepped seal with a ribbed casing is proposed to efficiently reduce the leakage at the...
Dogu, Yahya/0000-0003-0474-2899WOS: 000371125300016Conventional labyrinth seal applications in turbo...
This paper includes results of experimental research and CFD calculations concerning gas flow in seg...
ASME Turbo Expo: Turbine Technical Conference and Exposition -- JUN 15-19, 2015 -- Montreal, CANADAD...
Unsteady flow phenomena in turbomachinery are a source of aerodynamic losses and can adversely affec...
As well known, the stability assessment of turbomachines is strongly related to internal sealing com...
Secondary flows in turbomachinery highly affect the overall efficiency and rotorstability. A prime e...
Due to the character of the original source materials and the nature of batch digitization, quality ...
Typescript (photocopy).A computational/experimental study was conducted on the incompressible flow i...
Straight-through labyrinth seal is a simple and reliable noncontact seal structure widely used in ae...
The leakage between rotational and stationary part is one of the main source of performance loss in ...
Due to the character of the original source materials and the nature of batch digitization, quality ...
3noWhen numerically simulating the performance of a complete Francis turbine, it is common practice...
The reliable prediction of the effect of various labyrinth parameters on leakage rate has not been r...
The most important issue when designing the labyrinth sealing knots is the question of the correctne...
A new type of stepped seal with a ribbed casing is proposed to efficiently reduce the leakage at the...
Dogu, Yahya/0000-0003-0474-2899WOS: 000371125300016Conventional labyrinth seal applications in turbo...
This paper includes results of experimental research and CFD calculations concerning gas flow in seg...
ASME Turbo Expo: Turbine Technical Conference and Exposition -- JUN 15-19, 2015 -- Montreal, CANADAD...
Unsteady flow phenomena in turbomachinery are a source of aerodynamic losses and can adversely affec...
As well known, the stability assessment of turbomachines is strongly related to internal sealing com...
Secondary flows in turbomachinery highly affect the overall efficiency and rotorstability. A prime e...