文章基本信息

标题：Rolling Moment of Slender Body at High Incidence for Air to Air Missile Rocket Applications
其他标题：Rolling Moment of Slender Body at High Incidence for Air to Air Missile Rocket Applications
本地全文：下载
作者：Priyank Kumar
期刊名称：Defence Science Journal
印刷版ISSN：0976-464X
出版年度：2020
卷号：70
期号：1
页码：18-22
出版社：Defence Scientific Information & Documentation Centre
摘要：Measurements of moments were carried out on a slender body having a pointed forebody at lower velocities. The slender body had an ogive nose shape and an overall length to diameter ratio of 16. The angle of incidence was varied from low to moderate angles of attack in the pitch plane. The main objective of the present investigation was to measure the rolling moments on the slender body with and without the control technique. The side force was reduced using a rectangular cross-sectioned ringplaced suitably on the body, however, the slender body was found to experience rolling moments which may be catastrophic.
关键词：Asymmetric vortex;Side force;Rolling moment;Rings