弯尾弹头的网格外形设计及气动特性工程计算

Grid Contour Design and Aerodynamic Feature Engineering Computation for Bend -tail Warhead

弯尾导弹是提高导弹机动性的重要技术方案之一。本文研究了弯尾导弹的外形设计和网格生成方法,设计了导弹的几何外形。并对弯尾导弹的设计特点、网格生成技术、高超声速常规气动设计作了初步探讨。

The band -tail missile is one of the im portant technical proposals to im-prove the maneuverability of the mis sile.This paper researched the bend-tail missile contour design and grid generation method,and designed the geographic c ontour of the missile.And also it made a preliminary discussion over the bend -tail mis sile design feature,grid generation technique and high supersonic conventional aerodynamic design.