Supersonic micro-jet of straight micro-tube exit
The experimental investigations on the phenomenon of supersonic flow at the exit of straight micro-tubes with diameters ranging from 150 to 530 μm were conducted. The successive incident and reflected shock wave on supersonic and under-expanded flow were visualized by the Shadowgraph and Schlieren...
Gorde:
| Egile Nagusiak: | , , , , |
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| Formatua: | Artigo |
| Hizkuntza: | Inglês |
| Argitaratua: |
The Japan Society of Mechanical Engineers
2015-12-01
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| Saila: | Journal of Thermal Science and Technology |
| Gaiak: | |
| Sarrera elektronikoa: | https://www.jstage.jst.go.jp/article/jtst/10/2/10_2015jtst0026/_pdf/-char/en |
| Etiketak: |
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