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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
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2021
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Article
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Fig 11
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Research Article
Effects of Heat Addition on Wave Drag Reduction of a Spiked Blunt Body
Figure 11
Mach contours in a limited range from 0 to 1 of the M6 case. (a) M6_spike, (b) M6_spike_q1, (c) M6_spike_q2, and (d) M6_spike_q3.
(a)
(b)
(c)
(d)