1. An airfoil in a free stream where P- = 0.61 atm, p- = 0.819 Kg/m2, and V- = 300 m/s. At a point on the airfoil surface, the pressure is 0.5 atm. Assuming isentropic flow, calculate the velocity at that point.
1. An airfoil in a free stream where P- = 0.61 atm, p- = 0.819 Kg/m2, and V- = 300 m/s. At a point on the airfoil surface, the pressure is 0.5 atm. Assuming isentropic flow, calculate the velocity at that point.
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Transcribed Image Text:Assignment No. 1
1. An airfoil in a free stream where P = 0.61 atm, p- = 0.819 Kg/m3, and V. = 300 m/s. At a point on the airfoil
surface, the pressure is 0.5 atm. Assuming isentropic flow, calculate the velocity at that point.
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