SUMMARY OF AN ACTIVE FLEXIBLE WING PROGRAM

被引：60

作者：

PERRY, B

COLE, SR

MILLER, GD

机构：

[1] Aeroelasticity Branch, Structures Division, M/S 340, NASA Langley Research Center, Hampton, VA

[2] North American Aircraft, M/SGB01, Rockwell International Corporation, Los Angeles, CA, 90009

来源：

JOURNAL OF AIRCRAFT | 1995年 / 32卷 / 01期

关键词：

D O I：

10.2514/3.46677

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

This article presents a summary of a NASA/Rockwell Active Flexible Wing program. Major elements of the program are presented. Keg program accomplishments included single- and multiple-mode flutter suppression, load alleviation and load control during rapid roll maneuvers, and multi-input/multi-output multiple-function active controls tests above the open-loop flutter boundary.

引用

页码：10 / 15

页数：6

共 19 条

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[2]

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[9]

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[10]

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