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A Calculation Method of Rolling Characteristics of Canard Missile with Free-Spinning Tails

Ping'an Liu Mingyuan Liu

哈尔滨工业大学学报（英文版）2019，Vol.26Issue(6)：62-68,7.

哈尔滨工业大学学报（英文版）2019，Vol.26Issue(6)：62-68,7.DOI:10.11916/j.issn.1005-9113.18093

A Calculation Method of Rolling Characteristics of Canard Missile with Free-Spinning Tails

Ping'an Liu ¹Mingyuan Liu¹

作者信息

1. College of Aerospace and Civil Engineering, Harbin Engineering University, Harbin 150001, China
折叠

摘要

关键词

numerical simulation/canard missile/free-spinning tail/wind tunnel test/rolling characteristics

Key words

numerical simulation/canard missile/free-spinning tail/wind tunnel test/rolling characteristics

分类

军事科技

引用本文复制引用

Ping'an Liu,Mingyuan Liu..A Calculation Method of Rolling Characteristics of Canard Missile with Free-Spinning Tails[J].哈尔滨工业大学学报（英文版）,2019,26(6):62-68,7.

基金项目

Sponsored by the Fundamental Research Funds for the Central Universities (Grant No. HEUCFG201815). （Grant No. HEUCFG201815）

哈尔滨工业大学学报（英文版）

ISSN：1005-9113

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