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.

(a)

(b)

(c)

(d)

(e)

(f)

(g)

(h)

(i)