Although the overall effect of compressor fouling on engine performance has been recognized for many years, remarkably little has been published on the quantifiable effects. Mathematical modelling of compressors using stage stacking methods has recently been used for a systematic study of compressor fouling and earlier investigations led to an interest in the effects of engine size and compressor stage loading. This paper presents a proposed index showing the susceptibility of compressors to fouling, which could be useful in helping operators to determine cleanup intervals. Three engines of widely differing performance were used in developing this index and additional operator experience would be useful in confirming its validity
The fouling of axial flow compressors and turbines is a serious operating problem in gas turbine e...
Gas turbine performance degradation over time is mainly due to the deterioration of compressor and t...
The study of the adhesion of micro sized particles to gas turbine internal surfaces, commonly known ...
Fouling is the most important performance degradation factor, so it is necessary to accurately predi...
Gas turbine axial compressor performance are heavily influenced by blade fouling; as a result, the g...
The file attached to this record is the author's final peer reviewed version. The Publisher's final ...
Gas turbine axial compressor performance is heavily influenced by blade fouling. As a result, the ga...
In this paper, three-dimensional numerical simulations are carried out to evaluate the effect of f...
It is commonly accepted that fouling degrades severely axial compressor performance. Deposits build ...
none3noGas turbine axial compressor performance are heavily influenced by blade fouling; as a resul...
Three-dimensional numerical simulations of the effect of fouling on an axial compressor stage were c...
Gas turbine axial compressor performance is heavily influenced by blade fouling; as a result, the ga...
which permits unrestricted use, distribution, and reproduction in any medium, provided the original ...
In this paper, three-dimensional numerical simulations are carried out to evaluate the effect of fou...
Gas turbine axial compressor performance is heavily influenced by blade fouling; as a result, the ga...
The fouling of axial flow compressors and turbines is a serious operating problem in gas turbine e...
Gas turbine performance degradation over time is mainly due to the deterioration of compressor and t...
The study of the adhesion of micro sized particles to gas turbine internal surfaces, commonly known ...
Fouling is the most important performance degradation factor, so it is necessary to accurately predi...
Gas turbine axial compressor performance are heavily influenced by blade fouling; as a result, the g...
The file attached to this record is the author's final peer reviewed version. The Publisher's final ...
Gas turbine axial compressor performance is heavily influenced by blade fouling. As a result, the ga...
In this paper, three-dimensional numerical simulations are carried out to evaluate the effect of f...
It is commonly accepted that fouling degrades severely axial compressor performance. Deposits build ...
none3noGas turbine axial compressor performance are heavily influenced by blade fouling; as a resul...
Three-dimensional numerical simulations of the effect of fouling on an axial compressor stage were c...
Gas turbine axial compressor performance is heavily influenced by blade fouling; as a result, the ga...
which permits unrestricted use, distribution, and reproduction in any medium, provided the original ...
In this paper, three-dimensional numerical simulations are carried out to evaluate the effect of fou...
Gas turbine axial compressor performance is heavily influenced by blade fouling; as a result, the ga...
The fouling of axial flow compressors and turbines is a serious operating problem in gas turbine e...
Gas turbine performance degradation over time is mainly due to the deterioration of compressor and t...
The study of the adhesion of micro sized particles to gas turbine internal surfaces, commonly known ...