IMECH-IR  > 高温气体动力学国家重点实验室
零攻角NADTPS重构高超声速流场气动力/热研究
韩桂来; 姜宗林
Source Publication第十四届全国激波与激波管学术会议论文集(上册).中国安徽黄山.2010-07-14,p.288-293
2010-07-14
Pages288-293
Conference Name第十四届全国激波与激波管学术会议论文集(上册)
Conference Place中国安徽黄山
Abstract长时间、远距离高超声速飞行要求飞行器设计兼顾减阻和防热特点,论文提出无烧蚀自适应减阻防热新概念(NADTPS)并展开相关研究。NADTPS基于支杆-钝头体结构重构流场,利用侧向射流重点防护支杆头部。本文通过数值求解二维轴对称Navier-Stokes方程,对零攻角下NADTPS重构流场进行模拟,研究流场基本特征、气动力/热特性,分析新概念的减阻和防热机理。
Keyword减阻防热系统 高超声速 流场重构 气动力/热 数值模拟
Funding Organization国家自然科学基金(90916028)的资助
URL查看原文
Language中文
Document Type会议论文
Identifierhttp://dspace.imech.ac.cn/handle/311007/44167
Collection高温气体动力学国家重点实验室
Corresponding Author韩桂来
Recommended Citation
GB/T 7714
韩桂来,姜宗林. 零攻角NADTPS重构高超声速流场气动力/热研究[C],2010:288-293.
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