Question: Need help with this problem CoursHeroTranscribedText: Problem 1: (40 points total) Consider a circular cylinder in a hypersonic ow: with its axis perpendicular to the

Need help with this problem

CoursHeroTranscribedText: Problem 1: (40 points total) Consider a circular cylinder in a hypersonic ow: with its axis perpendicular to the flow. Let gt be the angle measured between radii drawn to the leading edge (the stagnation point) and to any arbitrary point on the cylinder. The pressure coeicient. distribution along the cylindrical surface is given by GP : 20032g3) for 0 g cf) g 7T/2 and 37r/2 g (,5 g 271' and CF : O for 7r/ 2 3 gt 3 371' / 2. Calculate the drag coeicient for the cylinder, based 011 projected frontal area of the cylinder

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