Abstract: Forced response is a common aeroelastic problem which can lead to blade damage. The computational fluid dynamics/computational structural dynamics (CFD/CSD) simulation is the most accurate numerical method to analyze the ...

Abstract: In transonic flow, nonlinear problems due to shock waves could be induced by gusts, leading to difficulty in acquiring a relatively accurate aerodynamic model in the form of a state equation for gust alleviation, which is ...

Abstract: The hypothesis of a conventional traveling wave model cannot cover the aerodynamic coupling effect of tandem blade cascades, while the aerodynamic interference between the front and rear blades of the cascade has a remarkable ...

Abstract: At present, autonomous driving decision-making solutions take few elements into account while ignoring the unpredictable nature of driving behavior, which makes it challenging to manage complicated traffic situations. To ...

Abstract: This paper proposed an extended state observer (ESO)-based discrete-time sliding-mode controller (DSMCer) to improve the steady-state output tracking accuracy of the systems with unmeasurable states and unknown mismatched ...