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Supersonic micro-jet of straight micro-tube exit

Published:2015 Issue:2 Volume:10 Page:JTST0026-JTST0026
ISSN:1880-5566
Container-title:Journal of Thermal Science and Technology
language:en
Short-container-title:JTST

Author:

HONG Chungpyo¹,YOSHIDA Yasuhiro²,MATSUSHITA Shinichi²,UENO Ichiro²,ASAKO Yutaka³

Affiliation:

1. Department of Mechanical Engineering, Kagoshima University

2. Department of Mechanical Engineering, Tokyo University of Science

3. Department of Mechanical Precision Engineering, Malaysia-Japan International Institute of Technology, University Technology Malaysia

Publisher

Japan Society of Mechanical Engineers

Subject

Engineering (miscellaneous),Instrumentation,General Materials Science,Atomic and Molecular Physics, and Optics

Link

https://www.jstage.jst.go.jp/article/jtst/10/2/10_2015jtst0026/_pdf

Reference12 articles.

1. Addy, A. L., Effect of Axisymmetric Sonic Nozzle Geometry on Mach Disk Characteristics, AIAA Journal, Vol. 19 (1998), pp. 121-122.

2. Asako, Y., Nakayama, K. and Shinozuka T., Effect of Compressibility on Gaseous Flows in a Micro-tube, International Journal of Heat and Mass Transfer, Vol. 48 (2005), pp. 4985-4994.

3. Aniskin, V., Mironov, S. and Maslov, A., Investigation of the structure of supersonic nitrogen microjets, Microfluid Nanofluid, Vol. 14 (3-4) (2013), pp. 605-614.

4. Baek, S. C., Kwon, A. B., Kim, H. D., Setoguchi, T. and Matuo, S., Study of Moderately Underexpanded Supersonic Moist Air Jets, AIAA Journal, Vol. 44(7) (2006), pp. 1624-1627.

5. Cumber, P. S., Fairweather, M., Falle, S. A. E. G. and Giddings, J. R., Prediction of Structure of Turbulent, Highly Underexpanded Jets, Journal of Fluids Engineering, Vol. 117 (1995), pp. 599-604.

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