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The Scientific World Journal
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2013
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Article
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Fig 6
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Research Article
Unstart Coupling Mechanism Analysis of Multiple-Modules Hypersonic Inlet
Figure 6
Static pressure contours mixing with streamlines of cross section
in a buzz cycle.
(a)
(b)
(c)
(d)
(e)
(f)
(g)
(h)
(i)