Add to ORKGA one-dimensional theory regarding the change of state in a multistage axial compressor at design point and part load has been formulated. With regard to short calculation times for obtaining compressor maps this algorithm is suitable to get insight into the main parameters influencing the off-design behaviour. An 'academic' test example, representing a 3-stage subsonic compressor, has been used for tests
A comparison between two different methods for aerodynamic calculation of multistage axial compresso...
A comparison between two different methods for aerodynamic calculation of multistage axial compresso...
This paper focuses on the development of an algorithm for designing an axial flow compressor for a p...
A one-dimensional theory regarding the change of state in a multistage axial compressor at design po...
Stage stacking methods commonly use a one-dimensional (1D) through flow analysis at the mean line to...
An axial compressor loss and deviation model that was developed and presented during previous resear...
The object of the present paper is to present a fast and reliable CFD tool that is able to simulate ...
Design and adjustment of compressors at modern gas-turbine engines are based on the wide use of nume...
Gas turbine operating state determination consists of the assessment of the modification, due to det...
PART I: An analysis of a multi-stage axial compressor with high reaction blading is carried out...
Gas turbine operating state determination consists of the assessment of the modification, due to det...
The development of a reliable mathematical model of an axial compressor requires applying flow and e...
Axial compressors are widely used in many aerodynamic applications. The design of an axial compresso...
For use in computing the detailed performance parameters of individual blade rows of a multistage co...
This study focuses on predicting axial compressor stage characteristics using a single performance p...
A comparison between two different methods for aerodynamic calculation of multistage axial compresso...
A comparison between two different methods for aerodynamic calculation of multistage axial compresso...
This paper focuses on the development of an algorithm for designing an axial flow compressor for a p...
A one-dimensional theory regarding the change of state in a multistage axial compressor at design po...
Stage stacking methods commonly use a one-dimensional (1D) through flow analysis at the mean line to...
An axial compressor loss and deviation model that was developed and presented during previous resear...
The object of the present paper is to present a fast and reliable CFD tool that is able to simulate ...
Design and adjustment of compressors at modern gas-turbine engines are based on the wide use of nume...
Gas turbine operating state determination consists of the assessment of the modification, due to det...
PART I: An analysis of a multi-stage axial compressor with high reaction blading is carried out...
Gas turbine operating state determination consists of the assessment of the modification, due to det...
The development of a reliable mathematical model of an axial compressor requires applying flow and e...
Axial compressors are widely used in many aerodynamic applications. The design of an axial compresso...
For use in computing the detailed performance parameters of individual blade rows of a multistage co...
This study focuses on predicting axial compressor stage characteristics using a single performance p...
A comparison between two different methods for aerodynamic calculation of multistage axial compresso...
A comparison between two different methods for aerodynamic calculation of multistage axial compresso...
This paper focuses on the development of an algorithm for designing an axial flow compressor for a p...