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COMPUTATIONAL STUDY OF SUPERSONIC FLOW PAST BLUNTED TANGENT-OGIVE NOSE CONE

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Figure

Fig. 1: Variation of Pressure coefficient with upper body of a blunted tangent ogive (r/R =0.4, and ρ
Fig. 2: Variation of Mach number with position along the axis of a blunted tangent ogive at r/R = 0.4 (r = 10 mm, R = 25mm) for (a)100mm (b)150mm (c)200mm (d)250mm

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