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What is the formula for coefficient of drag over a circular cylinder at hypersonic speed?(a) cd = \(\frac {D}{q_∞ S}\)(b) cd = \(\frac {D}{2q_∞ S}\)(c) cd = \(\frac {2D}{q_∞ S}\)(d) cd = Dq∞SThis question was posed to me during an online exam.Question is taken from Time-Marching Technique topic in section Time-Marching Technique of Aerodynamics |
Answer» Right CHOICE is (a) cd = \(\frac {D}{q_∞ S}\) |
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