Experimental Study of Single Expansion Ramp Nozzle Performance Using Pitot Pressure and Static Pressure Measurements

<div>Oblique shock waves of the compression section. (a) Schlieren photography for the compression section. (b) Mach number contours for the compression section.</div>

International Journal of Aerospace Engineering

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Figure 6

Figure 6: Experimental Study of Single Expansion Ramp Nozzle Performance Using Pitot Pressure and Static Pressure Measurements 