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Strength and Frequency of Underwater Shock Waves Related to Sterilization Effects on a Marine Bacterium Read chapter Read first chapter

2019 | OriginalPaper | Chapter

Ballistic Range Experiment and Numerical Simulation of Shock Stand-Off Distances Over Spheres in CO2

Authors : Dongjun Liao, Sen Liu, Jie Huang, Hexiang Jian, Aimin Xie, Zonghao Wang

Published in: 31st International Symposium on Shock Waves 2

Publisher: Springer International Publishing

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Abstract

To provide experimental data for validation of numerical simulations, measurement of shock stand-off distances over spheres in CO2 has been made in the hypervelocity ballistic range of Hypervelocity Aerodynamics Institute, China Aerodynamic Research and Development Center. The models were spheres with a diameter of 10 mm. The flight speeds were between 2.122 km/s and 4.220 km/s, with ambient pressures between 2.42 kPa and 12.3 kPa. The shock stand-off distance was measured using shadowgraph. Results revealed that high-temperature gas effect is more obvious in CO2 than in air, while two-temperature nonequilibrium model can basically reproduce the shock stand-off distances over spheres under present test conditions. The flow over spheres of present test is speculated to be mainly nonequilibrium. The accuracy and capability of two-temperature nonequilibrium model in CO2 may differ with different flow speeds and pressures, which need to be further investigated.

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Metadata
Title
Ballistic Range Experiment and Numerical Simulation of Shock Stand-Off Distances Over Spheres in CO2
Authors
Dongjun Liao
Sen Liu
Jie Huang
Hexiang Jian
Aimin Xie
Zonghao Wang
Copyright Year
2019
Book
31st International Symposium on Shock Waves 2

Print ISBN: 978-3-319-91016-1

Electronic ISBN: 978-3-319-91017-8

Copyright Year: 2019

DOI
https://doi.org/10.1007/978-3-319-91017-8_119

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