International audienceBrush seals are a mature technology that has generated extensive experimental and theoretical work. Theoretical models range from simple correlations with experimental results to advanced numerical approaches coupling the bristles deformation with the flow in the brush. The present work follows this latter path. The bristles of the brush are deformed by the pressure applied by the flow, by the interference with the rotor and with the back plate. The bristles are modeled as linear beams but a nonlinear numerical algorithm deals with the interferences. The brush with its deformed bristles is then considered as an anisotropic porous medium for the leakage flow. Taking into account, the variation of the permeability with t...
We attempt in this paper to develop a model for the flow through brush seals and determine their ela...
Dogu, Yahya/0000-0003-0474-2899WOS: 000253484200031The industrial applications of brush seals have b...
Dogu, Yahya/0000-0003-0474-2899WOS: 000237463200017Pressure and flow fields lay at the basis of such...
Dogu, Yahya/0000-0003-0474-2899WOS: 000371125300019Brush seals require custom design and tailoring d...
International Gas Turbine Institute, ASME2003 ASME Turbo Expo -- 16 June 2003 through 19 June 2003 -...
48th International Gas Turbine and Aeroengine Congress and Exhibition -- JUN 16-19, 2003 -- ATLANTA,...
This paper presents a brief history of the development of brush seals and their use in propulsive an...
In this paper an experimental programme and a CFD based mathematical model using a brush seal at two...
Dogu, Yahya/0000-0003-0474-2899WOS: 000444148300014Developments in brush seal analyses tools have be...
International audienceis paper presents a brief review of the experimental and theoretical state of ...
International Gas Turbine InstituteASME Turbo Expo 2017: Turbomachinery Technical Conference and Exp...
Aerodynamic resistance of a brush seal was mainly studied. The velocity distribution along three spe...
International audienceThe paper presents the experimental results obtained for brush seals of 38 mm ...
ASME Turbo Expo: Turbine Technical Conference and Exposition -- JUN 15-19, 2015 -- Montreal, CANADAD...
Abstract: One of the theoretical approaches to modelling brush seals is based on the porous medium m...
We attempt in this paper to develop a model for the flow through brush seals and determine their ela...
Dogu, Yahya/0000-0003-0474-2899WOS: 000253484200031The industrial applications of brush seals have b...
Dogu, Yahya/0000-0003-0474-2899WOS: 000237463200017Pressure and flow fields lay at the basis of such...
Dogu, Yahya/0000-0003-0474-2899WOS: 000371125300019Brush seals require custom design and tailoring d...
International Gas Turbine Institute, ASME2003 ASME Turbo Expo -- 16 June 2003 through 19 June 2003 -...
48th International Gas Turbine and Aeroengine Congress and Exhibition -- JUN 16-19, 2003 -- ATLANTA,...
This paper presents a brief history of the development of brush seals and their use in propulsive an...
In this paper an experimental programme and a CFD based mathematical model using a brush seal at two...
Dogu, Yahya/0000-0003-0474-2899WOS: 000444148300014Developments in brush seal analyses tools have be...
International audienceis paper presents a brief review of the experimental and theoretical state of ...
International Gas Turbine InstituteASME Turbo Expo 2017: Turbomachinery Technical Conference and Exp...
Aerodynamic resistance of a brush seal was mainly studied. The velocity distribution along three spe...
International audienceThe paper presents the experimental results obtained for brush seals of 38 mm ...
ASME Turbo Expo: Turbine Technical Conference and Exposition -- JUN 15-19, 2015 -- Montreal, CANADAD...
Abstract: One of the theoretical approaches to modelling brush seals is based on the porous medium m...
We attempt in this paper to develop a model for the flow through brush seals and determine their ela...
Dogu, Yahya/0000-0003-0474-2899WOS: 000253484200031The industrial applications of brush seals have b...
Dogu, Yahya/0000-0003-0474-2899WOS: 000237463200017Pressure and flow fields lay at the basis of such...