Wing rock analysis of slender delta wings, review and extension

被引：18
作者：
Ericsson, LE
机构：
[1] Mt. View, CA
来源：
JOURNAL OF AIRCRAFT | 1995年 / 32卷 / 06期
关键词：
D O I：
10.2514/3.46867
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
An analysis of existing experimental results, performed to pinpoint the flow physics of slender wing rock, especially in regard to the roles played by vortex liftoff and vortex breakdown, revealed that the influence of roll-rate-induced conical camber as well as of model support and wind-tunnel wall interference could be surprisingly large.
引用
收藏
页码：1221 / 1226
页数：6
相关论文
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