APPLICATION OF NLR's CALCULATION METHODS TO TRANSONIC FLOW ABOUT OSCILLATING WINGS.

被引：0

作者：

Hounjet, M.H.L. ^{[1
]}

van der Kolk, J.T. ^{[1
]}

Meijer, J.J. ^{[1
]}

机构：

[1] Natl Aerospace Lab, Dep of, Aeroelasticity, Amsterdam, Neth, Natl Aerospace Lab, Dep of Aeroelasticity, Amsterdam, Neth

来源：

Journal of Aircraft | 1985年 / 22卷 / 12期

关键词：

AERODYNAMIC LOADS - FIGHTER CONFIGURATION - NATIONAL AEROSPACE LABORATORY (NLR) - OSCILLATING WINGS - TRANSONIC TRANSPORT WING MODEL;

D O I：

暂无

中图分类号：

学科分类号：

摘要：

引用

页码：1034 / 1042

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