高超声速风洞HSCM系列标准模型气动力实验数据  

Aerodynamic Test Data of HSCM Calibration Models in Hypersonic Wind Tunnel

作　　者：张婷婷 叶瑞 姜维[1] 陈星[1] ZHANG Ting-ting;YE Rui;JIANG Wei;CHEN Xing(China Academy of Aerospace Aerodynamics, Beijing 100074, China)

机构地区：[1]中国航天空气动力技术研究院,北京100074

出　　处：《气体物理》2021年第4期57-65,共9页Physics of Gases

摘　　要：在风洞建成运行初期和风洞实验技术与CFD技术的不断发展过程中,风洞标模实验一直都有特别重要的现实意义.汇总了近5年FD-07风洞HSCM系列标模实验的结果,针对HSCM系列AGARD HB-2标模、尖锥10°标模、AGARD B标模,给出了系统、全面、详实、可靠的实验数据,为相关实验和计算的评估提供借鉴和参考.In the initial stage of wind tunnel construction and operation,as well as in the continuous development of wind tunnel test technology and CFD technology,wind tunnel calibration model tests have always been of great practical significance.The experiment results of HSCM series calibration models in FD-07 hypersonic wind tunnel in recent five years were summarized,including the AGARD HB-2 calibration model,sharp cone calibration model with half-angle of 10°and AGARD-B calibration model.Systemic,comprehensive,elaborate and reliable experiment data of the calibration models were presented,which can provide reference for evaluation of relevant experiments and computations.

关 键 词：高超声速风洞 标模 HSCM HB-2 尖锥 AGARD-B 

分 类 号：V211.74[航空宇航科学与技术—航空宇航推进理论与工程]