彭治雨, 石义雷, 龚红明, 李中华, 罗义成
CJA
收稿日期:2014-07-23
修回日期:2014-10-08
出版日期:2015-01-15
发布日期:2014-10-09
通讯作者:
彭治雨,Tel.: 0816-2465017 E-mail: pengzhiyu65536@163.com
E-mail:pengzhiyu65536@163.com
作者简介:彭治雨 男,硕士,研究员。主要研究方向:高超声速气动热研究。 Tel: 0816-2465017 E-mail: pengzhiyu65536@163.com
PENG Zhiyu, SHI Yilei, GONG Hongming, LI Zhonghua, LUO Yicheng
Received:2014-07-23
Revised:2014-10-08
Online:2015-01-15
Published:2014-10-09
摘要：
高超声速气动热预测技术是高超声速飞行器发展的关键技术之一。对高超声速气动热预测技术的发展情况进行了分析探讨。首先,简要回顾了国内外高超声速气动热理论预测及地面实验技术的发展历程;在此基础上,结合典型外形的计算与风洞试验结果的比较,重点介绍分析了气动热工程计算方法、数值模拟方法、气动热风洞试验设备的模拟能力及目前实验测试技术的研究水平;最后,对气动热预测技术的发展趋势进行了讨论,提出了气动热预测技术应研究解决的问题。
中图分类号:
彭治雨, 石义雷, 龚红明, 李中华, 罗义成. 高超声速气动热预测技术及发展趋势[J]. 航空学报, 2015, 36(1): 325-345.
PENG Zhiyu, SHI Yilei, GONG Hongming, LI Zhonghua, LUO Yicheng. Hypersonic aeroheating prediction technique and its trend of development[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(1): 325-345.
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