标签副翼颤振问题的非线性解

IF 1.4 4区工程技术 Q2 ENGINEERING, AEROSPACE

Aeronautical Journal Pub Date : 1970-06-01 DOI:10.1017/S0001924000114812

D. L. Birdsall

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引用次数: 2

摘要

在这十年里，飞机设计程序涉及的分析显示出越来越高的准确性，以满足日益增长的操作需求，妥协的边界迅速收敛于可接受的范围也就不足为奇了。一架成品飞机成为一个明确定义的设计问题的唯一解决方案，或者更可怕的是，它成为一个独特问题的解决方案。如果在解决方案产生后问题发生了变化……这就是生活。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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A Non-Linear Solution to a Tab-Aileron Flutter Problem

In a decade when aircraft design procedures involve analyses which display ever increasing accuracy to satisfy growing operational demands, it is not surprising that the boundaries of compromise rapidly converge upon the envelope of acceptability. A finished aircraft becomes the unique solution to a well-defined design problem–or what is even more frightening, it becomes a solution to a unique problem. If the problem changes after the solution has been produced… c'est la vie.

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来源期刊

Aeronautical Journal 工程技术-工程：宇航

CiteScore

3.70

自引率

14.30%

发文量

审稿时长

6-12 weeks

期刊介绍： The Aeronautical Journal contains original papers on all aspects of research, design and development, construction and operation of aircraft and space vehicles. Papers are therefore solicited on all aspects of research, design and development, construction and operation of aircraft and space vehicles. Papers are also welcomed which review, comprehensively, the results of recent research developments in any of the above topics.