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The NATO STO AVT-201 Task Group on Extended Assessment of Stability an Control Prediction Methods for NATO Air Vehicles: Summary

机译:北约STO AVT-201稳定性扩展评估任务组和北约飞行器的控制预测方法:摘要

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摘要

This article presents cross-comparisons of the results obtained within the NATO STO AVT-201 Extended Assessment of Reliable Stability & Control Prediction Method for NATO Air and Sea Vehicles Task Group. The results of five participating organizations and six different CFD solvers are compared to the available wind tunnel data from the DNW-NWB wind tunnel obtained at low Mach number, for both static and dynamic cases. The comparisons help to find commonalities and disparities in the CFD predictions of the aerodynamics of a generic UCAV, SACCON, and point to areas where CFD is challenged by non-linear aerodynamics flow prediction. These comparisons help to show where the modeling and simulation of novel aircraft platforms in the earliest stages of design development can contribute to a more successful design process by determining difficult non-linear aerodynamics and helping to change the design prior to the later stages of the design process.
机译:本文介绍了在北约STO AVT-201对北约空中和海上飞行器任务组的可靠稳定性和控制预测方法的扩展评估中获得的结果的交叉比较。对于静态和动态情况,将五个参与组织和六个不同的CFD求解器的结果与以低马赫数获得的DNW-NWB风洞的可用风洞数据进行比较。这些比较有助于发现通用UCAV,SACCON的空气动力学的CFD预测中的共性和差异,并指出非线性空气动力学流量预测对CFD提出挑战的领域。这些比较有助于显示在设计开发的最早阶段,新型飞机平台的建模和仿真可以通过确定困难的非线性空气动力学特性并在设计的后期阶段之前进行更改来促进更成功的设计过程。过程。

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