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Pusher-Propeller Blade Loading With and Without Pylon Trailing-Edge Blowing

机译:带有和不带有定向塔后缘吹气的推进器-螺旋桨叶片加载

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摘要

The aerodynamic interaction e_ects characteristic of pusher propellers were studied at the Large Low-Speed Facility of the German{Dutch wind tunnels (DNW-LLF). A propeller model was positioned downstream of a pylon equipped with a trailing-edge blowing system. Surface-pressure transducers integrated into the propeller blades con_rmed the local impact of the pylon wake on the blade loads. At an intermediate thrust setting, the sectional lift impulsively increased by 30% during the wake passage. The application of pylon blowing decreased the integral velocity de_cit in the pylon wake by up to 77% compared to the unblown case. As a result, the load uctuations during the wake encounter were practically eliminated, thereby mitigating the adverse installation e_ects.
机译:在德国{荷兰风洞(DNW-LLF)“的大型低速设施中研究了推进器螺旋桨的空气动力相互作用特性。螺旋桨模型位于配备了后缘吹气系统的塔架的下游。集成在螺旋桨叶片中的表面压力传感器确认了塔式尾流对叶片载荷的局部影响。在中等推力设定下,在尾流通过期间,截面升力脉冲增加了30%。与未吹塑的情况相比,施加塔架吹塑可使塔架尾流中的整体速度下降达77%。结果,实际上消除了遇到尾流期间的载荷波动,从而减轻了不利的安装影响。

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