International Journal of Aerospace Engineering / 2017 / Article / Fig 15

Research Article

Experimental Study on Aerodynamic Heating Induced by Dual Injections into Hypersonic Cross Flow

Figure 15

Comparison of half width of region A induced by single and tandem dual injection(s) with each injection hole spacing. Plots indicate loci of maximum St in region A on each position. indicates the freestream direction.
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