Design of a continuously variable Mach-number nozzle

作     者：郭善广 王振国 赵玉新 GUO Shan-guang;WANG Zhen-guo;ZHAO Yu-xin

作者机构：Science and Technology on Scramjet Laboratory National University of Defense Technology 

基　　金：Project(11072264)supported by the National Natural Science Foundation of China 

出 版 物：《Journal of Central South University》 (中南大学学报（英文版）)

年 卷 期：2015年第22卷第2期

页      码：522-528页

摘      要：A design method was developed to specify the profile of the continuously variable Mach-number nozzle for the supersonic wind tunnel. The controllable contour design technique was applied to obtaining the original nozzle profile, while other Machnumbers were derived from the transformation of the original profile. A design scheme, covering a Mach-number range of3.0

主 题 词：设计方法 无级变速 马赫数 喷嘴 计算流体动力学 超音速风洞 均匀流动 配置文件 

学科分类：0810[工学-土木类] 0806[工学-电气类] 080103[080103] 08[工学] 080104[080104] 0805[工学-能源动力学] 0703[理学-化学类] 0812[工学-测绘类] 0801[工学-力学类] 

核心收录：

D　O　I：10.1007/s11771-015-2551-5

馆 藏 号：203751308...