Journal of Projectiles, Rockets, Missiles and Guidance >
Research on Aerodynamic Characteristics of Missile with Deflectable Nose Control
Received date: 2013-06-20
Online published: 2025-05-30
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.
WANG Lin , FAN Wentao , GAO Yuan . Research on Aerodynamic Characteristics of Missile with Deflectable Nose Control[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2014 , 34(2) : 123 -126 . DOI: 10.15892/j.cnki.djzdxb.2014.02.033
| [1] | Goddard R H Apparatus for steering aircraft: US, 2594766[P]. 1952. |
| [2] | Thomson K D The use of a deflectable nose on a missile as a control device WSRL-0211-TR[R]. Defense Research Centre Salisbury, 1981. |
| [3] | Thomson K D Wind tunnel tests on a tube-launched missile configuration with a deflectable nose control and a novel wrap-around fin stabilizer, WSRL-0327-TR[R]. Defense Research Centre Salisbury, 1983. |
| [4] | Landers MG, Hall LH. Deflectable nose and canard controls for a fin-stabilized projectile at supersonic and hypersonic speeds, AIAA 2003 – 3805 [R], 2003. |
| [5] | Richardson Doug UK systems house displays 'Droop Snoot' missile concept[J]. Jane's Missiles and Rockets, 2002, 6(9): 1. |
| [6] | US Army Proposes 'Droop-Snoot' Missile Guidance[J]. Jane's Missiles and Rockets, 2003,7 (1): 15. |
| [7] | Berry RP, Lawless DF, Cayson S C, et al. Magnetostrictive missile guidance system: US: 6467722 [P].2002. |
| [8] | Justin Mullins You can run, but you cant hide[J]. New Scientist, 1997. |
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