Cavitation is a widespread and detrimental phenomenon in hydraulic machinery, therefore,
it requires to be accurately predicted. In this study, large eddy simulation (LES), scale …

The next generation of ultrahigh bypass ratio civil aero-engines promises notable engine
cycle benefits. However, these benefits can be significantly eroded by a possible increase in …

Aiming at the aeroelastic stability of labyrinth seal ring under intake distortion condition, a
numerical model for the aeroelastic stability of labyrinth seal ring with intake distortion was …

Aeroelastic phenomena in the low-pressure compression (LPC) system of civil turbofan
engines can cause a significant high-cycle fatigue (HCF) risk to the LPC components …

With the startup of the aero-engine, the ground vortex is formed between the ground and the
engine intake. The ground vortex leads to total pressure and swirl distortion, which reduces …

An einem für aeroakustische Untersuchungen entwickelten Labor-Fan-Prüfstand wurden
detaillierte aerodynamische und aeroakustische Messungen mit verschiedenen …

The design of aero-engine intakes for compact nacelles can be an important contributor in
achieving cruise fuel burn reductions. A key aspect for the design of viable compact intakes …

Predicting the resonant forced response of aero-engine fans from inlet distortions in
crosswind conditions is challenging, primarily due to the difficulty in correctly characterising …