高超音速飞行器及其关键技术简论  

A REVIEW ON HYPERSONIC VEHICLES AND KEY TECHNOLOGIES

作　　者：杨亚政[1] 李松年[1] 杨嘉陵[1] 

机构地区：[1]北京航空航天大学

出　　处：《力学进展》2007年第4期537-550,共14页Advances in Mechanics

基　　金：北京市教育委员会工程力学共建项目资助(XK100060522)

摘　　要：简要评述了高超音速飞行器及其关键技术,包括:高超音速飞行的定义、高超音速流动的特征、高超飞行覆盖范围、高超飞行器蒙皮温度、以及高超飞行设计特点;高超飞行器的背景;高超飞行器研制的发展简史,及经验与思考;吸气式高超飞行器典型设计过程、发展战略、技术规划、和关键技术领域.This paper begins with a classical definition of hypersonic, some physical phenomena pertinent to hypersonic flight, the covered range of the hypersonic flight and the features of design process. The differences between AHV（hypersonic airbreathing vehicles） and RHV（hypersonic rocket vehicles） are discussed, with a table showing temperatures. In the second part, the paper puts hypersonic vehicles in a military background. A historical perspective of hypersonic vehicles is given in form of a table with milestones, accompanied with some lessons learned from the past and relevant for the future. In the last part, a typical design process, development strategy, technology program, and key technologies of hypersonic airbreathing vehicles are reviewed.

关 键 词：高超音速流动 吸气式高超飞行器 涡轮发动机冲压喷气发动机 涡轮基组合循环 火箭基组合循环 热防护系统 

分 类 号：V271[航空宇航科学与技术—飞行器设计]