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A real-time hybrid aeroelastic simulation platform for flexible wings

机译:用于柔性机翼的实时混合气动弹性仿真平台

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The concept of real-time hybrid aeroelastic simulation for flexible wings is introduced in this paper. In a hybrid aeroelastic simulation, a coupled aeroelastic system is "broken down" into an aerodynamic simulation subsystem and a structural vibration subsystem. The coupling between structural dynamics and aerodynamics is maintained by the real-time communication between the two subsystems. As the vibration of the testing article (a wing member or a full aircraft) is actuated by actuators, hybrid aeroelastic simulation and experiment can eliminate the sizing constraint of the conventional aeroelastic testing performed within a wind-tunnel. It also significantly saves the cost of wind-tunnel testing. However, several critical technical problems (such as process noise, measurement noise, and actuator delay) need to be addressed to enable a hybrid simulation in real-time. This paper proves the concept of real-time hybrid simulation and discusses some of the critical problems underlying the technique. (C) 2019 Elsevier Masson SAS. Ali rights reserved.
机译:介绍了柔性机翼实时混合气动弹性仿真的概念。在混合气动弹性模拟中,耦合的气动弹性系统被“分解”为一个气动模拟子系统和一个结构振动子系统。结构动力学与空气动力学之间的耦合通过两个子系统之间的实时通信来保持。由于测试物品(机翼部件或整个飞机)的振动由致动器驱动,因此混合气动弹性仿真和实验可以消除风洞内进行的常规气动弹性测试的尺寸限制。这也大大节省了风洞测试的成本。但是,需要解决一些关键的技术问题(例如过程噪声,测量噪声和执行器延迟),以实现实时混合仿真。本文证明了实时混合仿真的概念,并讨论了该技术背后的一些关键问题。 (C)2019 Elsevier Masson SAS。阿里权利保留。

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