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Research on the Influence of Wing Structure Parameters on Aerodynamic Characteristics of Single-blade Terminal-sensitive Projectile
Received date: 2016-03-21
Online published: 2025-05-23
In order to research the influence law of the single-blade terminal-sensitive projectile on its aerodynamic characteristics, based on commercial software Ansys Fluent, the influence law of wing's length, width, tip mass and rotating angle on drag coeffiecient, rotating moment coeffiecient and pitching moment coeffiecient was studied in detail. The results showed that the aerodynamic parameters increased linearly with the increase of wing length and width. Wing's tip mass slightly affected on aerodynamic parameters, while the wing's rotating angle strongly affected on aerodynamic parameters which presented parabolic variation.
JIANG Tao , GUO Rui , LIU Rongzhong . Research on the Influence of Wing Structure Parameters on Aerodynamic Characteristics of Single-blade Terminal-sensitive Projectile[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2017 , 37(1) : 91 -94 . DOI: 10.15892/j.cnki.djzdxb.2017.01.021
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