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Vibro-acoustic analysis of flight test data comprising fuselage vibrations, external pressure and interior cabin noise measurements

机译:包括机身振动,外部压力和室内舱噪声测量的飞行试验数据的振动声学分析

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In the yean 2011 and 2012, a series of flight tests with DLR's A320-232 research aircraft 'D-ATRA' were carried out within the German national (LuFo IV) project SIMKAB with the objective to improve cabin acoustics comfort in passenger aircrafts. In order to study the source mechanisms responsible for aircraft cabin noise, an extensive flight test campaign was carried out that considered multiple flight and operational conditions of the aircraft. For the global analysis of this problem, structure-borne noise as well as airborne sound sources must be considered. Hence, an extensive data set was collected that consists of vibration measurements of the fuselage primary structure and cabin interior, unsteady surface-pressure for characterization of the turbulent boundary layer, engine induced external sound pressure and sound pressure inside the cabin. In total, 154 vibration signals, 38 unsteady pressure signals, 80 external microphones and 66 internal microphones have been used in more than 300 different flight conditions. In the current paper, the main focus is given to the medium frequency range and in particular to the vibration analysis since the acceleration of the fuselage acts as an intermediate element between sources and receivers. The different flight conditions evaluated considered different flight speeds, flight levels, engine operation conditions, etc The analysis included, among others, the correlation of ail acquired data in order to investigate the energy transfer mechanisms. Results show consistency of the expected relation between dynamic pressure and vibro-acoustic responses for such problem. Evidence indicates a clear structure-borne influence of engine related vibrations at low frequencies, whereas cabin noise at middle-high frequencies is driven by the turbulent boundary layer. This project was supported by the Federal Ministry for Economic Affairs and Energy on the basis of a decision by the German Bundestag.
机译:在Yean 2011和2012年,与DLR A320-232研究飞机'D-ATRA的一系列飞行试验在德国国家(Lufo IV)项目Simkab中进行了目的,以改善客机的客舱声学舒适性。为了研究负责飞机舱噪声的源机制,进行了广泛的飞行测试活动,被考虑了飞机的多个飞行和操作条件。对于解决此问题的全局分析,必须考虑结构传播的噪音以及空中声源。因此,收集了广泛的数据集,该数据集由机身初级结构和机舱内部,不稳定的表面压力进行振动测量,用于表征湍流边界层,发动机引起外部声压和机舱内的声压。总共为154个振动信号,38个不稳定的压力信号,80个外部麦克风和66个内部麦克风在300多个不同的飞行条件下使用。在本发明的纸张中,主焦点被赋予中等频率范围,特别是振动分析,因为机身的加速充当源和接收器之间的中间元件。不同的飞行条件评估被认为是不同的飞行速度,飞行水平,发动机操作条件等,其中包括AIL获取数据的相关性以研究能量转移机制。结果显示了对这种问题的动态压力和振动声反应之间的预期关系的一致性。证据表明发动机相关振动在低频下的明显结构对,而中高频率的驾驶室噪声由湍流边界层驱动。该项目是由德国联邦钢茶的决定的基础上的联邦经济事务和能源的支持。

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