Aerodynamic Heating Characteristics Over a Protuberance in Hypersonic Flows Using Fast Response Thermo Gauges-Reference-Cited by-同舟云学术

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Aerodynamic Heating Characteristics Over a Protuberance in Hypersonic Flows Using Fast Response Thermo Gauges

Published:2010-09-15 Issue:3 Volume:11 Page:193-200
ISSN:2093-274X
Container-title:International Journal of Aeronautical and Space Sciences
language:en
Short-container-title:International Journal of Aeronautical and Space Sciences

Author:

Lee Hyoung-Jin,Lee Bok-Jin,Jeung In-Seuck,Kim Seoung-Lyoung,Kim In-Sun

Publisher

The Korean Society for Aeronautical & Space Sciences

Link

http://ocean.kisti.re.kr/downfile/crosscheck/ksass/JAKO201028552430393.pdf

Cited by 7 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Correction of inertance of temperature sensing devices in high-speed flow;Journal of Physics: Conference Series;2019-11-01

2. Fast response co-axial thermocouple for short duration impulse facilities;Applied Thermal Engineering;2016-03

3. Investigation of the separated region ahead of three-dimensional protuberances on plates and cones in hypersonic flows with laminar boundary layers;Physics of Fluids;2014-12

4. Hypersonic interference heating on cones with short three-dimensional protuberances;Experimental Thermal and Fluid Science;2014-05

5. Hypersonic Interference Heating on Flat Plate with Short Three-Dimensional Protuberances;AIAA Journal;2014-04

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