Design and testing of a blended wing body aeroelastic wind-tunnel model

被引：6

作者：

Carlsson, M ^{[1
]}

Kuttenkeuler, J ^{[1
]}

机构：

[1] Kungliga Tekniska Hogskolan, Dept Aeronaut, Div Flight Dynam, SE-10044 Stockholm, Sweden

来源：

JOURNAL OF AIRCRAFT | 2003年 / 40卷 / 01期

关键词：

Blended wing body (BWB) transport aircrafts;

D O I：

10.2514/2.3079

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

(Edited Abstract)

引用

页码：211 / 213

页数：3

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