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Aerodynamic interference between high-speed slender bodies

机译:高速细长体之间的气动干扰

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摘要

Significant aerodynamic interference can occur between high-speed bodies in close proximity. A complex flowfield develops where shock and expansion waves from a generator body impinge upon the adjacent receiver body. The pressure and flow angularity changes which occur across these disturbances modify the body aerodynamics. The aim of this research is to quantify the aerodynamic interference effects for multi-body configurations and understand the relevant flow physics. The interference aerodynamics for slender bodies in a supersonic flow were investigated through a parametric wind tunnel study. The receiver bodies were finned and un-finned configurations. The effect of lateral and axial body separations, receiver incidence and the strength of the disturbance field were investigated. Measurements included forces and moments, surface pressures and flow visualisations. Supporting computations using steady-state, viscous predictions provided a deeper understanding of the underlying aerodynamics and flow mechanisms. Good agreement was found between the measured and predicted interference loads and surface pressures for all configurations. The interference loads are strongly dependent upon the axial impingement location of the primary shockwave. These induced loads change polarity as the impingement location moves aft over the receiver. The magnitude of the interference loads increase when the receiver is at incidence and are amplified by up to a factor of three when rear fins are attached. In general, the interference loads are larger for a stronger disturbance flowfield. The centre of pressure location is substantially affected and the static stability of the finned receiver changes in some configurations. The effect of the aerodynamic interference on the body trajectories was assessed using an unsteady, Euler prediction in combination with a 6DOF dynamic model. This shows aerodynamic ii interference can cause a collision between the bodies. Moreover, the initial interference loads dominate the subsequent body trajectories and static modelling can be used to evaluate the dynamic trajectories.
机译:紧密靠近的高速车身之间可能会发生明显的空气动力学干扰。形成复杂的流场,其中来自发电机主体的冲击波和膨胀波撞击到相邻的接收器主体上。在这些扰动上发生的压力和流量角度变化会改变人体的空气动力学。这项研究的目的是量化多体配置的气动干扰效应,并了解相关的流动物理学。通过参数风洞研究,研究了超音速流动中细长物体的干扰空气动力学。接收器主体为有鳍和无鳍配置。研究了横向和轴向物体分离,接收器入射和干扰场强度的影响。测量包括力和力矩,表面压力和流动可视化。使用稳态粘性预测进行的支持计算可提供对基本空气动力学和流动机理的更深入的了解。在所有配置的实测和预测干扰载荷与表面压力之间都发现了很好的一致性。干扰载荷在很大程度上取决于主冲击波的轴向冲击位置。当撞击位置在接收器上向后移动时,这些感应的负载会改变极性。当接收器处于入射位置时,干扰负载的大小会增加,而在安装后鳍片时,干扰负载的大小会放大至三倍。通常,对于更强的干扰流场,干扰载荷更大。压力位置的中心受到显着影响,并且鳍状接收器的静态稳定性在某些配置中会发生变化。使用不稳定的Euler预测与6DOF动态模型相结合,评估了空气动力干扰对人体轨迹的影响。这表明空气动力ii的干扰会导致车身之间发生碰撞。此外,初始干扰载荷支配着随后的身体轨迹,并且可以使用静态建模来评估动态轨迹。

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