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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
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2016
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Article
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Fig 5
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Research Article
Numerical Investigation of Shock Wave Diffraction over a Sphere Placed in a Shock Tube
Figure 5
Description of the used grids: (a) has
points, (b)
points, and (c)
points; every 10th grid line is drawn.
(a)
(b)
(c)