机械科学与技术2012，Vol.31Issue(3)：350-352,3.
可水下发射飞行器载体头罩分离计算数学模型
A Mathematic Model Applied for the Hood Separation of Underwater Launching Aircraft′s Carrier
李涛 1宋保维1
作者信息
- 1. 西北工业大学航海工程学院,西安710072
- 折叠
摘要
Abstract
Underwater launching aircraft is a new unmanned aircraft which is carried,launched by an underwater vehicle,then moves in and exit the water,and flies in air eventually.For the hood separation of underwater launching aircraft,we proposed a separation design approach using circumferential and radial collocated cutting blasting considering the requirements of reliability and security.The mathematical model of the hood separation is established to calculate the hood separation characteristics and to predict the trajectory of separated bodies.The present study provides the necessary theoretical basis to the design of underwater launching aircraft.关键词
水下发射/载体/头罩分离/数学模型Key words
underwater launching/carrier/hood separation/mathematical model分类
军事科技引用本文复制引用
李涛,宋保维..可水下发射飞行器载体头罩分离计算数学模型[J].机械科学与技术,2012,31(3):350-352,3.
