The design and operation of gas-turbine engines is heavily influenced by the off-design stability of the compressor, which limits obtainable performance and may result in aeroelastic vibration issues. Whilst Variable Stator Vanes (VSVs) are widely used to mitigate this problem, research considering the mismatching effect of VSVs away from their optimal settings is limited. In this thesis, a high-speed variable geometry compressor is studied at part-speed conditions and VSV setting adjustments are made to deliberately trigger stable rotating stall and study its behaviour. Examination of unsteady measurements reveals two "families'' of rotating stall, each at different frequencies, where the dominant behaviour depends upon the VSV settin...
[EN] This paper presents the results of a computational investigation of the aerodynamic choking mec...
[EN] This paper presents the results of a computational investigation of the aerodynamic choking mec...
Work on rotating stall and its related disturbances has been in progress since the Second World War....
Variable Stator Vanes (VSVs) are commonly used in multi-stage axial compressors for stage matching a...
A three dimensional unsteady Reynolds-Averaged Navier-Stokes solver was used to perform multistage u...
The forcing functions and structural responses characterizing gas turbine rotor/case system vibratio...
A three dimensional unsteady Reynolds-Averaged Navier-Stokes solver was used to perform multistage u...
A three dimensional unsteady Reynolds-Averaged Navier-Stokes solver was used to perform multistage u...
Variable Stator Vanes (VSVs) are commonly used in multistage axial compressors for stage matching at...
A three dimensional unsteady Reynolds-Averaged Navier-Stokes solver was used to perform m...
A three dimensional unsteady Reynolds-Averaged Navier-Stokes solver was used to perform m...
In this paper, research that was carried out to optimise an initial variable guide vane schedule of...
Variable geometry blade rows are a common instrument to avoid compressor instabilities which occur e...
Variable geometry blade rows are a common instrument to avoid compressor instabilities which occur e...
April 1995Includes bibliographical references (page 21)This paper presents the results from a set of...
[EN] This paper presents the results of a computational investigation of the aerodynamic choking mec...
[EN] This paper presents the results of a computational investigation of the aerodynamic choking mec...
Work on rotating stall and its related disturbances has been in progress since the Second World War....
Variable Stator Vanes (VSVs) are commonly used in multi-stage axial compressors for stage matching a...
A three dimensional unsteady Reynolds-Averaged Navier-Stokes solver was used to perform multistage u...
The forcing functions and structural responses characterizing gas turbine rotor/case system vibratio...
A three dimensional unsteady Reynolds-Averaged Navier-Stokes solver was used to perform multistage u...
A three dimensional unsteady Reynolds-Averaged Navier-Stokes solver was used to perform multistage u...
Variable Stator Vanes (VSVs) are commonly used in multistage axial compressors for stage matching at...
A three dimensional unsteady Reynolds-Averaged Navier-Stokes solver was used to perform m...
A three dimensional unsteady Reynolds-Averaged Navier-Stokes solver was used to perform m...
In this paper, research that was carried out to optimise an initial variable guide vane schedule of...
Variable geometry blade rows are a common instrument to avoid compressor instabilities which occur e...
Variable geometry blade rows are a common instrument to avoid compressor instabilities which occur e...
April 1995Includes bibliographical references (page 21)This paper presents the results from a set of...
[EN] This paper presents the results of a computational investigation of the aerodynamic choking mec...
[EN] This paper presents the results of a computational investigation of the aerodynamic choking mec...
Work on rotating stall and its related disturbances has been in progress since the Second World War....