Limit cycle oscillation characteristics of fighter aircraft

被引：84

作者：

Bunton, RW ^{[1
]}

Denegri, CM

机构：

[1] USN, Air Warfare Ctr, Div Aircraft,Flight Test Engn Grp, Strike Aircraft Test Directorate, Patuxent River, MD 20670 USA

[2] USAF, SEEK EAGLE Off, Engn Branch, Certificat Div, Eglin AFB, FL 32542 USA

来源：

JOURNAL OF AIRCRAFT | 2000年 / 37卷 / 05期

关键词：

D O I：

10.2514/2.2690

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

An overview is given on the basic nature of LCO and the evolution of the terminology. Some observed distinctions and similarities between limit cycle oscillations (LCO) and classical flutter are presented. Further, the impacts of LCO on test procedures, aircraft store certification, and mission capability are discussed.

引用

页码：916 / 918

页数：3