波音777高升力气动设计概述

IF 1.4 4区工程技术 Q2 ENGINEERING, AEROSPACE

Aeronautical Journal Pub Date : 1995-11-01 DOI:10.1017/S0001924000028670

B. N. Nield

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引用次数: 52

摘要

摘要介绍了波音777飞机高升力系统的设计过程。特别注意设计上的限制，并举例说明已完成的贸易研究。介绍了理论设计工具和实验测试程序。介绍了大升力元件的概况，并将飞行试验结果与预测结果进行了比较。

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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An overview of the Boeing 777 high lift aerodynamic design

Abstract The process of designing the Boeing 777 high lift system is described. Particular attention is given to design constraints and examples are given of the trade studies completed. The theoretical design tools and experimental test program are described. A survey of the high lift elements is presented and flight test results are compared with predictions.

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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.