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Effects of atmospheric turbulence on large-span aircraft.

机译:大气湍流对大跨度飞机的影响。

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There is extensive interest in High Altitude Long Endurance (HALE) unmanned air vehicles (UAV), used for atmospheric research, as pseudo-satellite systems, and for military C3I. Typical of this class is the Helios, a solar powered UAV of 245 ft wingspan designed and built by AeroVironment, Inc. as part of the Environmental Research Aircraft and Sensor Technology (ERAST) project funded by NASA. Because of its spanloader design, the wing is lightly loaded under normal cruise and G-Loads and experiences its most severe loading cases in turbulence of spanwise scale comparable to the wing. Existing gust load and turbulence models are deceptively conservative because they do not deal with the spanwise varying excitation. This research is funded by a grant from NASA Langley Research Center.; An initial fundamental aero-elastic model (the unitary mode) has been developed for the case of flexural deformation only, ignoring pitch. This model is the basis of the design of the AeroVironment, Inc. flight vehicles. A more realistic model, incorporating torsional deformations as well as flexural (the binary mode) has been developed. Exact solutions for excitation of any wave number and reduced frequency case are derived using Sears and Theodorsen models for unsteady airfoil loads. The bending moment transfer function shows that the maximum bending moment occurs for spanwise waves approximately equal to span, and that the contribution of flightwise only turbulence is minimal.; Sensitivity studies are made using a representative spanloader, identifying the effect of altitude, turbulence length scale, and stiffness. They show that wing flexibility reduces the turbulence loads by about 20% compared with those on a rigid wing.; Predictions of the response have been plotted against actual flight test data taken from initial Helios Missions. The flight data involves tests of limited periods and relatively low altitude, so that is not comprehensive. Subject to the restricted data the theory developed here shows good agreement with the experiments and supports the assumptions of the present model.
机译:对于用于大气研究,伪卫星系统和军用C3I的高海拔长期耐力(HALE)无人飞行器(UAV)引起了广泛兴趣。此类飞机中最典型的就是Helios,这是一架245英尺翼展的太阳能无人机,由AeroVironment,Inc.设计和制造,是NASA资助的环境研究飞机和传感器技术(ERAST)项目的一部分。由于翼展装载机的设计,机翼在常规巡航和G载荷下承受的载荷很小,并且在与翼展相当的翼展尺度湍流中承受着最严重的载荷情况。现有的阵风载荷和湍流模型在外观上是保守的,因为它们不处理跨度变化的激励。这项研究由NASA兰利研究中心资助。最初的基本空气弹性模型(单一模式)仅针对挠曲变形而忽略了节距而开发。该模型是AeroVironment,Inc.飞行器设计的基础。已经开发了一种更现实的模型,该模型包含了扭转变形以及弯曲(二进制模式)。对于不稳定的翼型载荷,使用Sears和Theodorsen模型得出了用于激发任何​​波数和低频情况的精确解。弯矩传递函数表明,最大弯矩发生在大约等于跨度的翼展波上,并且仅沿飞行方向的湍流贡献最小。使用代表性的跨距装载机进行灵敏度研究,确定高度,湍流长度比例和刚度的影响。他们表明,与刚性机翼相比,机翼的柔韧性使湍流负荷降低了约20%。已根据从最初的Helios任务获得的实际飞行测试数据绘制了响应的预测。飞行数据涉及有限时间和相对较低高度的测试,因此并不全面。在受限数据的约束下,本文开发的理论与实验结果吻合良好,并支持本模型的假设。

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