Research on Aerodynamic Characteristics of Missile with Deflectable Nose Control
Received date: 2013-06-20
Online published: 2025-05-30
王辚 , 范文涛 , 高原 . 偏转弹头导弹气动特性研究[J]. 弹箭与制导学报, 2014 , 34(2) : 123 -126 . DOI: 10.15892/j.cnki.djzdxb.2014.02.033
A computational investigation has been completed at Mach number of 2, 3, and 4 to compare the aerodynamic characteristics and pitch control effectiveness of missile with deflectable nose and canard controls. The computation results indicate that compared with canard control, deflectable nose control has strong points in aerodynamics, control effectiveness and maneuverability, the control efficiency increases as the Mach number increases. Thus deflectable nose control is a perfect control method of hypersonic missile.
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