Add to ORKGEffects of unsteady flow interactions on the aerodynamic performance of a highly-loaded transonic axial compressor are investigated in the present study. The primary focus of the study is to investigate how unsteady flow interactions between blade rows affect the aerodynamic performance of a highly-loaded transonic axial compressor. Recent experimental and numerical studies of current highly-loaded axial compressor performance indicated that predicting calculating the loss generation is very challenging with various analysis tools. In the present study, the effects of generation and transport of shock induced vortices on the compressor performance is investigated in detail
Transonic compressors are regularly used as part of the compression system in industrial gas turbine...
AbstractNumerical investigation of the unsteady flow variability driven by rotor-stator interaction ...
Unsteady aerodynamics is becoming more and more important for future compressor improvements. It has...
The present paper reports an investigation of unsteady loss generation in the stator due to the inco...
The primary focus of this paper is to investigate the loss sources in an advanced GE transonic compr...
The performance of compressors and the sophistication of analysis tools have reached a level such th...
Although it is known that the flow field in a turbomachine is unsteady, current design tools do not ...
Gas turbine total pressure ratio, efficiency and accurate stage matching prediction are of increasin...
AbstractThe unsteady 3D flow fields in a single-stage transonic compressor under designed conditions...
Blade row interaction effects on loss generation in compressors have received increased attention as...
Experiments are performed in an advanced design 1&1/2 stage high-speed axial compressor to investiga...
Rotor wake dispersion in a low-speed, one and half stage axial compressor is investigated in detail ...
April 1980Also issued as: Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronauti...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 2008.Includes...
In the present study, unsteady flow behavior in a modern transonic axial compressor rotor is studied...
Transonic compressors are regularly used as part of the compression system in industrial gas turbine...
AbstractNumerical investigation of the unsteady flow variability driven by rotor-stator interaction ...
Unsteady aerodynamics is becoming more and more important for future compressor improvements. It has...
The present paper reports an investigation of unsteady loss generation in the stator due to the inco...
The primary focus of this paper is to investigate the loss sources in an advanced GE transonic compr...
The performance of compressors and the sophistication of analysis tools have reached a level such th...
Although it is known that the flow field in a turbomachine is unsteady, current design tools do not ...
Gas turbine total pressure ratio, efficiency and accurate stage matching prediction are of increasin...
AbstractThe unsteady 3D flow fields in a single-stage transonic compressor under designed conditions...
Blade row interaction effects on loss generation in compressors have received increased attention as...
Experiments are performed in an advanced design 1&1/2 stage high-speed axial compressor to investiga...
Rotor wake dispersion in a low-speed, one and half stage axial compressor is investigated in detail ...
April 1980Also issued as: Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronauti...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 2008.Includes...
In the present study, unsteady flow behavior in a modern transonic axial compressor rotor is studied...
Transonic compressors are regularly used as part of the compression system in industrial gas turbine...
AbstractNumerical investigation of the unsteady flow variability driven by rotor-stator interaction ...
Unsteady aerodynamics is becoming more and more important for future compressor improvements. It has...