Research Article
Numerical Simulation of Supersonic Carman Curve Bodies with Aerospike
Figure 11
Flowfield features in Mach number 2. (a) and , pressure contour. (b) and , pressure contour. (c) and , pressure contour. (d) and , velocity contour. (e) and , velocity contour. (f) and , velocity contour. (g) , pressure curves (h). and , pressure lines. (i) and , streamlines.
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