Question: Consider a wing inside the test section of a subsonic wind tunnel. The velocity of the air flow is 1 6 0 f t s

Consider a wing inside the test section of a subsonic wind tunnel. The velocity of the air flow is 160fts. If the velocity at a point on the wing is 195fts, what is the pressure coefficient at the point on the wing? What is the pressure coefficient at the tip of the pitot-tube? If the flow velocity is increased to 650fts and test section temperature reading is 510R, what is the pressure coefficient on the same point?
Consider a wing inside the test section of a

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