The purpose of this paper is to perform a numerical study regarding the implementation of
dielectric barrier discharge plasma micro-actuators for load alleviation on a NACA 23012 …

This paper studies how to control boundary slope of optimized parts in density-based
topology optimization for additive manufacturing (AM). Boundary slope of a part affects the …

We report work done to investigate the adaptability of the end wall unsteady pulsed jet (UPJ)
at different incidence angles. In this research, the influence of the UPJ on the cascade …

Tandem blade configurations are said to being able to outperform conventional single
blades in terms of loss behaviour and flow turning. The work presented here is supported by …

Air injection is an effective method to eliminate flow separation and improve blade loading in
compressors. In existing studies on unsteady air injection, achieving a better control effect …

A dynamic mode decomposition (DMD) is carried out for the flow field in a compressor
cascade with plasma actuators employed for aeroelastic control. Numerical assessments …

Virtual control surfaces are assessed numerically as a means to enhance the aeroelastic
response of a compressor cascade. Virtual surfaces are realized with plasma actuators …

Based on unsteady numerical simulation, the feasibility of utilizing a fluid oscillator to
generate oscillating jets for relieving the compressor cascade's corner separation was …

With the aim of deepening the understanding of high-speed compressor cascade flow, this
paper reports an experimental study on NACA-65 K48 compressor cascade with high …

A typical high-speed compressor cascade flow is simulated using an eddy viscosity model
and a Reynolds stress model. Based on comparisons with experimental results, the …