文章基本信息

标题：Oscillatory aerodynamic forces for a pitching aircraft
本地全文：下载
作者：R. R. Aggarwal
期刊名称：Defence Science Journal
印刷版ISSN：0976-464X
出版年度：2014
卷号：11
期号：1
页码：12-14
DOI：10.14429/dsj.11.6789
语种：English
出版社：Defence Scientific Information & Documentation Centre
摘要：Chordwise aerodynamic strip derivatives for the swept back wing having bending-torsion degrees of freedom as modified by the aircraft simple harmonic pitching oscillations have been calculated.
关键词：Bending-torsion;Aerodynamic strip;Oscillations