Due to the high ratio of surface area to volume and the limitations of manufacturing
precision, the impact of wall temperature and heat transfer on the aerodynamic performance …

The squealer tip has significant influence on both the aerodynamic and heat transfer
characteristics of the high-pressure turbine blade. However, due to the complexity of …

In this study, a turbine cascade squealer tip is optimized by a multi-objective genetic
algorithm (MOGA) with varying squealer heights and tip cooling configurations. The three …

The trailing edge tip region has always been the most vulnerable part of high-pressure
turbine blade. The requirements for both aerodynamic efficiency and cooling effectiveness …

The wakes that occur periodically owing to blade rotation, affect the HTCDs (heat transfer
coefficient distributions) on the turbine blade tip and shroud. We investigated the wake …

Increased scrutiny on aviation's environmental footprint has precipitated a dramatic increase
in gas turbine technology development, with a focus on engine performance improvements …

The optimization of the turbine rotor tip geometry remains a vital opportunity to create more
efficient and durable engines. Balancing the aerodynamic and thermal aspects, while …

To optimize the inclined rim design, multi-objective optimization was numerically conducted
on the suction-side rim of the squealer tip in the GE-E3 rotor blade. The RANS equations …

Film cooling is one of the external cooling techniques that is widely applied to the hot-gas
path components of a gas turbine, forming a thin film of a coolant on the surface to prevent …

Recent research suggests that the cooling flow at transonic turbine tip has several unique
flow features such as the strong interaction with the base flow, the acceleration at divergent …