다중 슬릿으로부터 방출된 충격파들의 간섭현상Interaction of Shock Waves Discharged from Multiple Slits

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Interaction of shock waves discharged from the multiple slits is studied numerically and experimentally using the KAIST shock tube. Investigation is made on such distinct flow regions as flow entering the slits, flow in the narrow slits, flow in the vortex-shock interaction region, and the relatively uniform flow behind the shock front. Visualization of the shocks and vortices associated with the jets from the single, double, and multiple slits is made using the holographic interferometry and shadowgraphy, the images of which are compared with the numerical results.
Publisher
한국항공우주학회
Issue Date
2000-09
Language
Korean
Citation

한국항공우주학회지, v.28, no.6, pp.31 - 35

ISSN
1225-1348
URI
http://hdl.handle.net/10203/19268
Appears in Collection
AE-Journal Papers(저널논문)
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