In commercial aviation, efficiency improvements may be gained by aerodynamic
optimisation of its structural components, such as the intermediate compressor duct (ICD) …

This work presents an experimental and numerical investigation on the laminar-turbulent
transition and secondary flow structures in a Turbine Rear Structure (TRS). The study was …

For the CFD community the mesh generation is still one of the most important stages to
obtain a good flow solution based on the full Navier-Stokes equations. For turbomachinery …

采用雷诺平均Navier-Stokes 方程和Spalart-Allmaras 湍流模型, 对可控涡设计的1.5
级高负荷亚音速试验涡轮进行三维黏性数值模拟, 对叶栅内旋涡发展和损失机制进行全面研究和 …

The coupling effect of local components is common in buildings and results in energy loss
and local drag. This effect is significantly influenced by the shape and size of the …

In the present work, heat transfer within gas turbine applications are investigated
bothexperimentally and numerically. The main content concerns heat transfer and fluidflow …

A good aerodynamic design of the turbine rear structure (TRS) is crucial for improving
efficiency and reducing emissions from aero-engines. This paper presents a detailed …

The development of the geared and ultra-high bypass ratio engines has increased the
demands and operational envelope for the low-pressure system in commercial aircraft …

Influence of the surface geometry variations on the flow in a low-pressure turbine outlet
guide vane cascade is studied experimentally and numerically. Experiments are performed …

This paper presents the effects of an unshrouded low pressure turbine (LPT) onto the
following exit guide vane row (EGV). The measurement results were obtained in the …