Journal of Projectiles, Rockets, Missiles and Guidance >
Numerical Simulation of Rolling Characteristics on Canard Control Missile and Tail Control Missile
Received date: 2012-11-29
Online published: 2025-05-26
To research rolling characteristics of missiles of different configurations, three dimensional compressible Reynolds averaged Navier-Strokes numerical simulations were solved. The flow field of canard control missile and tailcontrol missile at asymmetric attitude was calculated. The two configurations' characteristics including the change of rolling moment, different pressure of section plane on wing and influence between fin and wing were To investigated. The simulation results show that when fin turns to control roll at asymmetric attitude, the downwash brings different influence on the two configurations.
Key words： rolling characteristics; numerical simulation; fin; wing; downwash
JING Daiyong , LI Jian . Numerical Simulation of Rolling Characteristics on Canard Control Missile and Tail Control Missile[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2013 , 33(4) : 53 -54,60 . DOI: 10.15892/j.cnki.djzdxb.2013.04.035
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