The aim of the project is to study the physics of the flow using commercial CFD code, a) In the casing treatment which affects efficiency and stall margin in the transonic axial flow compressor and optimize the casing treatment geometry for the same compressor. b) Investigating the unsteady flow in the transonic axial flow compressor including the effect of interaction between the fixed and rotating blade rows in turbo machines
The flow in the transonic front rotor stage of a multi-stage axial flow compressor with casing treat...
When designing a transonic multi-stage compressor it is desirable to keep the devel- opment cost low...
This paper deals with the numerical studies on the combined effect of tip clearance and axisymmetric...
This study deals with unsteady numerical simulation of casing treatment in a stage of an axial compr...
This study deals with unsteady numerical simulation of casing treatment in a stage of an axial compr...
A single-stage transonic axial compressor was equipped with a casing treatment, consisting of 3.5 ax...
This study deals with unsteady numerical simulation of casing treatment in a stage of an axial compr...
An advanced axial-slot casing treatment on a transonic compressor: A close look with computational f...
A transonic axial flow compressor undergoes severe vibrations due to instabilities like stall and su...
={Previous studies on circumferential groove casing treatments have shown that the effectiveness of ...
In the design process of compressors for gas turbines, the application of casing treatments showed a...
The flow in the blade tip vicinity of the transonic first stage of a multi-stage axial flow compress...
This article presents the study of casing treatments on an axial compressor stage for improving stab...
Gehäusestrukturierungen sind in der Lage den aerodynamischen Betriebsbereich schaufelspitzenkritisch...
While the effects of axisymmetric casing treatment on performance of an axial compressor stage have ...
The flow in the transonic front rotor stage of a multi-stage axial flow compressor with casing treat...
When designing a transonic multi-stage compressor it is desirable to keep the devel- opment cost low...
This paper deals with the numerical studies on the combined effect of tip clearance and axisymmetric...
This study deals with unsteady numerical simulation of casing treatment in a stage of an axial compr...
This study deals with unsteady numerical simulation of casing treatment in a stage of an axial compr...
A single-stage transonic axial compressor was equipped with a casing treatment, consisting of 3.5 ax...
This study deals with unsteady numerical simulation of casing treatment in a stage of an axial compr...
An advanced axial-slot casing treatment on a transonic compressor: A close look with computational f...
A transonic axial flow compressor undergoes severe vibrations due to instabilities like stall and su...
={Previous studies on circumferential groove casing treatments have shown that the effectiveness of ...
In the design process of compressors for gas turbines, the application of casing treatments showed a...
The flow in the blade tip vicinity of the transonic first stage of a multi-stage axial flow compress...
This article presents the study of casing treatments on an axial compressor stage for improving stab...
Gehäusestrukturierungen sind in der Lage den aerodynamischen Betriebsbereich schaufelspitzenkritisch...
While the effects of axisymmetric casing treatment on performance of an axial compressor stage have ...
The flow in the transonic front rotor stage of a multi-stage axial flow compressor with casing treat...
When designing a transonic multi-stage compressor it is desirable to keep the devel- opment cost low...
This paper deals with the numerical studies on the combined effect of tip clearance and axisymmetric...