Aircraft Flutter Prediction Analysis Method and Device
A predictive analysis, aircraft technology, applied in instruments, special data processing applications, electrical digital data processing, etc., can solve the problems of inaccuracy, low accuracy of flutter prediction and analysis, and achieve the effect of improving accuracy
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Embodiment 1
[0022] figure 1 It is a flow chart of the aircraft flutter prediction analysis method provided by Embodiment 1 of the present invention. This embodiment can be applied to perform flutter prediction analysis on a certain part of the aircraft structure (such as wings, empennages, etc.) or the overall structure. The method can be performed by The aircraft flutter prediction and analysis device can be implemented, and the device can be implemented by software and / or hardware, and cooperate with the excitation points and collection points configured on the aircraft structure to realize the analysis method. The method specifically includes the following steps:
[0023] Step 110, applying an input signal through an excitation point configured on the aircraft structure, and receiving an output signal through a collection point configured on the aircraft structure.
[0024] Wherein, the excitation point may be an excitation device configured on the aircraft structure for applying vibr...
Embodiment 2
[0052] figure 2 It is a schematic diagram of an aircraft flutter prediction and analysis device provided in Embodiment 2 of the present invention. The aircraft flutter prediction and analysis device provided in Embodiment 2 of the present invention is used to implement the aircraft flutter prediction and analysis method provided in Embodiment 1. Such as figure 2 As shown, the aircraft flutter prediction and analysis device provided in Embodiment 2 includes a signal application acquisition module 210, a nonlinear dynamic model establishment module 220, an unsteady aerodynamic model establishment module 230, an unsteady aerodynamic model reduction module 240 and a flow Solid coupling analysis module 250 .
[0053] The signal applying and collecting module 210 is used for applying input signals through excitation points arranged on the aircraft structure, and receiving output signals through the collecting points arranged on the aircraft structure.
[0054] The nonlinear dyn...
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