期刊： INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 2021; 38 (3)
Centrifugal compressors have been widely used in light-duty turboshaft engines and automotive turbochargers. One of the essential requirements for cen......
期刊： INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 2021; 38 (2)
Humpback whales possess bumpy tubercles on the leading edge of their flippers. Due to these leading edge tubercles, whales are able to produce high de......
期刊： INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 2021; 38 (3)
In order to describe how the variant BPR affects the flow performance, a qusi-2D fan model was proposed. In the model, the stage cumulative method was......
期刊： INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 2021; 38 (2)
Due to the epistemic uncertainty, it is difficult for the experts to give precise parameter values in Risk Priority Number (RPN) evaluations. To overc......
期刊： INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 2021; 38 (3)
Trailing edge slot film cooling is a widely used method for protecting the trailing edge of turbine blades from hot gas impingement. The structures th......
期刊： INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 2021; 38 (2)
The process of rotor speed variation under tiltrotor cruise state has been studied, and the integrated variable speed control method of tiltrotor base......
期刊： INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 2021; 38 (3)
A streamline curvature method based integrated throughflow analysis approach is newly developed to deal with component matching problems of variable c......
期刊： INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 2021; 38 (3)
As per few investigation in installed performance for variable cycle engines, an analysis scheme is proposed on the basis of integrating variable cycl......
期刊： INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 2021; 38 (1)
The part-load performance of gas turbine is of great importance due to the consideration of running time spent at part power, and Variable Geometry Tu......
期刊： INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 2021; 38 (1)
Based on the aerodynamic matching configuration between a core driven fan stage (CDFS) and high pressure compressor (HPC), matching state point correl......
期刊： INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 2021; 38 (1)
The physical characteristics of self-sustain shock oscillation and the key factors that affect the shock oscillation in turbine-based combined-cycle(T......
期刊： INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 2021; 38 (1)
Corner separation limits the increase of the aerodynamic loading in the compressor. Previous numerical studies indicate that the Blended Blade and End......
期刊： INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 2021; 38 (1)
For rotating machinery, during its running, direct measuring for vibration of rotating components is very difficult. To overcome this defect, we prese......
期刊： INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 2021; 38 (1)
This paper deals with the creep characteristics of the aircraft turbine disc material of nickel-base superalloy GH4169 under high temperature. From th......
期刊： INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 2021; 38 (1)
This present work is aimed at providing detailed understanding of the flow mechanisms in a highly loaded centrifugal compressor with different diffuse......
