Numerical Simulation of Supersonic Carman Curve Bodies with Aerospike

Figure 12

The flowfield feature of the A2 and basic model at three Mach numbers. (a) Pressure contour of the basic model at Mach number 1.5. (b) Pressure contour of the basic model at Mach number 2. (c) Pressure contour of the basic model at Mach number 3. (d) Pressure contour of A2 at Mach number 1.5. (e) Pressure contour of A2 at Mach number 2. (f) Pressure contour of A2 at Mach number 3. (g) Pressure curves of A2 head and basic model at three Mach numbers. (h) Pressure curves of A2 aerodisk tip at three Mach numbers.

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