Inverse Method Using Finite Strain Measurements to Determine Flight Load Distribution Functions

Cameron W. Coates; Priya Thamburaj

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Inverse Method Using Finite Strain Measurements to Determine Flight Load Distribution Functions

机译：使用有限应变测量来确定飞行载荷分布函数的逆方法

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摘要

This work seeks to identify in-flight loads based on real-time data provided by strain gauges. Flight loads are identified based on an inverse interpolation method that uses results from a finite element model developed in I-DEAS software. The inverse int

机译：这项工作旨在基于应变仪提供的实时数据来识别飞行中的负载。根据使用I-DEAS软件中开发的有限元模型结果的逆插值方法识别飞行载荷。逆整数

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来源
《Journal of Aircraft》 |2008年第2期|p.366-370|共5页
作者
Cameron W. Coates; Priya Thamburaj;
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作者单位

Armstrong Atlantic State University, Savannah, Georgia 31419;

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收录信息美国《科学引文索引》(SCI);美国《工程索引》(EI);
原文格式 PDF
正文语种 eng
中图分类航空;
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机译：利用飞行中应变测量确定航空航天器载荷和结构响应的逆插值方法

Inverse Method Using Finite Strain Measurements to Determine Flight Load Distribution Functions

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