With the continuous increase in aircraft flight altitude, low Reynolds number effects in high-
altitude environments significantly impact the stability of compressor operation. In this study …

The spike-type rotating stall in axial compressor is one of the major causes for the
aeroengine failure. The evolution of the flow structures, especially in the rotor tip region, is …

Safely operating compressors is quite critical. Rotating stall is highly undesirable and affects
negatively the performance and stability of aero-engine compressors. It is important to …

A novel approach to reduced-order modeling of high-dimensional systems with time-varying
properties is proposed. It combines the problem formulation of the Dynamic Mode …

The stable range of operation for the centrifugal compressor significantly influences the
dynamic, economic, and environment-friendly characteristics of power systems. A deep …

The tip-leakage vortex, as the dominant coherent structure of the blade tip of a compressor,
is an important source of losses in centrifugal compressor rotors; it limits the stall margin and …

The wave energy conversion of oscillation water column (OWC) systems is limited by the
narrow range of efficient operation of Wells turbines. Effective control methods are critical to …

Unsteady flow in the hub endwall region has long been a hot topic in the turbomachinery
community. However important it is to the performance of the whole engine, the coherent …

In this paper, higher-order dynamic mode decomposition (HODMD) was applied to find the
main patterns and frequencies of a transient aerodynamic flow field when an aircraft wing …

Research works over the years have identified a recirculating bubble locating at impeller
shroud in centrifugal compressor operating under off-design conditions. However, its roles …