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Overview of Recent Flight Flutter Testing Research at NASA Dryden

机译:NASA Dryden最近的飞行颤振测试研究概述

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摘要

In response to the concerns of the aeroelastic community, NASA Dryden Flight Research Center, Edwards, California, is conducting research into improving the flight flutter (including aeroservoelasticity) test process with more accurate and automated techniques for stability boundary prediction. The important elements of this effort so far include the following: (1) excitation mechanisms for enhanced vibration data to reduce uncertainty levels in stability estimates; (2) investigation of a variety of frequency, time, and wavelet analysis techniques for signal processing, stability estimation, and nonlinear identification; and (3) robust flutter boundary prediction to substantially reduce the test matrix for flutter clearance. These are critical research topics addressing the concerns of a recent AGARD Specialists' Meeting on Advanced Aeroservoelastic Testing and Data Analysis. This paper addresses these items using flight test data from the F/A-18 Systems Research Aircraft and the F/A-18 High Alpha Research Vehicle.
机译:为了响应航空弹性界的关注,位于加利福尼亚州爱德华兹的NASA德莱登飞行研究中心正在开展研究,以更加准确和自动化的技术来改进飞行颤振(包括航空弹性)测试过程,以进行稳定性边界预测。迄今为止,这项工作的重要内容包括:(1)增强振动数据的激励机制,以减少稳定性估计中的不确定性; (2)研究用于信号处理,稳定性估计和非线性识别的各种频率,时间和小波分析技术; (3)稳健的颤振边界预测,以大幅减少颤振间隙的测试矩阵。这些是关键的研究主题,旨在解决最近的AGARD专家会议关于高级航空气动弹性测试和数据分析的问题。本文使用F / A-18系统研究飞机和F / A-18高阿尔法研究飞行器的飞行测试数据来解决这些问题。

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