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Physics and Modeling of Large Flow Disturbances: Discrete Gust Encounters for Modern Air Vehicles
Annual Review of Fluid Mechanics ( IF 27.7 ) Pub Date : 2022-01-05 , DOI: 10.1146/annurev-fluid-031621-085520
Anya R. Jones 1 , Oksan Cetiner 2 , Marilyn J. Smith 3
Affiliation  

Gusts of moderate and large magnitude induce flow separation and other complexities when they interact with the lifting surfaces of air vehicles. The presence of these nonlinear gusts are becoming ubiquitous in twenty-first-century air vehicles, where the classic potential flow–based methodologies applied in the past may no longer be valid. In this review, we define the parameter space for the presence of large-amplitude gusts and describe where and when these gusts may primarily be found. Recent research using modern experimental and computational techniques to define the limits of classical unsteady and indicial aerodynamic theories is summarized, with a focus on discrete transverse, streamwise (longitudinal), and vortex gust encounters. We propose areas where future research is needed to transition these studies of large-amplitude gust physics to real-time prediction and mitigation during flight.

中文翻译:


大流量扰动的物理和建模:现代飞行器的离散阵风遭遇

当它们与飞行器的升力面相互作用时,中度和大强度的阵风会导致流动分离和其他复杂性。这些非线性阵风在 21 世纪的飞行器中变得无处不在,过去应用的基于势流的经典方法可能不再有效。在这篇综述中,我们定义了存在大振幅阵风的参数空间,并描述了这些阵风可能主要出现的地点和时间。总结了最近使用现代实验和计算技术来定义经典非定常和指示空气动力学理论的极限的研究,重点是离散的横向、流向(纵向)和涡旋阵风遭遇。

更新日期:2022-01-06
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