The application discloses a kind of hot aerodynamic elastic
system across
saddle transition dynamics stability
analysis method, comprising: S1, construct nonlinearly heated wallboard aeroelastic
system analysis model, obtain the buckling
modal configuration and vibration
modal configuration of linearized
system;S2, construct the reduced-order analysis model of nonlinearly heated wallboard aeroelastic system, for analyzing the stability characteristics of system initial equilibrium position;S3, construct the
potential energy surface of heated wallboard structure, for analyzing the
balance point species, quantity and position of wallboard under different temperatures;S4, consider aerodynamic elastic effect and load
aerodynamic load to construct the linearized across
saddle transition dynamics analysis model of hot aeroelastic system, for analyzing the across
saddle transition dynamics characteristics of multi-stable non-conservative dynamic system saddle point local jump behavior.The application realizes high-fidelity prediction to the nonlinear thermal aeroelastic behavior of wallboard structure, provides key theoretical tool for the thermal strength reliable design and accurate evaluation of wallboard structure.