A Calculation Method of Rolling Characteristics of Canard Missile with Free-Spinning Tails |
| |
Affiliation: | College of Aerospace and Civil Engineering, Harbin Engineering University, Harbin 150001, China |
| |
Abstract: | The steady flow field of a canard missile on different angles of attack and Mach numbers were studied. Based on analysis, a method was proposed to reduce the calculation for the rolling characteristics of the canard missile with free-spinning tails, and was tested to obtain the relations between rolling moment coefficient, Mach number, and angle of attack. All the computed rolling moment coefficients obtained from the proposed method greatly agreed with the experimental results of FD-06 wind tunnel in CAAA, which proved that the method can not only reduce the calculation cost but also keep precision in calculating the rolling characteristics of canard missiles. |
| |
Keywords: | numerical simulation canard missile free-spinning tail wind tunnel test rolling characteristics |
本文献已被 CNKI 万方数据 等数据库收录! |
| 点击此处可从《哈尔滨工业大学学报(英文版)》浏览原始摘要信息 |
|
点击此处可从《哈尔滨工业大学学报(英文版)》下载全文 |