This paper presents a multidisciplinary design optimization of a turbocharger radial turbine
for automotive applications with the aim to improve two major manufacturer requirements …

Enlarging the range of human displacement is a need in a globalized World where the
commercial, cultural or even recreational links between distinct human settlements are more …

Accurate predictions of unsteady forcing on turbine blades are essential for the avoidance of
high-cycle-fatigue issues during turbine engine development. Further, if one can …

A numerical method was used to investigate the reaction degree effects on the aerodynamic
performance and flow structure of the single-stage transonic turbine. The SST-γ-θ turbulence …

This paper presents a 3-D optimization of a moderately loaded transonic compressor rotor
by means of a multi-objective optimization system. The latter makes use of a Differential …

In a high-pressure turbine that is used in combination with a contrarotating low-pressure
turbine, the geometry of the low-pressure turbine guide vane gives rise to a shock reflection …

摘要为降低以气流加速为主要做功手段的零预旋涡轮动叶激波损失, 提出了以折转角为控制变量
的吸力面无遮盖段内凹型线量化设计方法. 根据激波等强度时波系总损失最小的原理 …

Single-stage high-pressure turbines often operate in the transonic regime, resulting in strong
shock interactions between the vanes and the rotor blades. With the present study, a Multi …

Aerodynamic design of an aero-engine fan blade is a multi-step process with multi-
variables. The general purpose in aerodynamic design is to obtain proper blade angles and …

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