Calculate the equivalent plate length for turbulent boundary

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Reference no: EM131515298

Question: A thin plate of length 1.0 m is held in a uniform air flow such that its length is parallel to the flow direction. The flow speed is 25 m/s, the viscosity, µ = 14.96 × 10-6 Pa/s, and the air density, 1.203 kg/m3.

(a) If it is known that transition from laminar to turbulent flow occurs when the Reynolds number based on x reaches 500,000, find the transition point.

(b) Calculate the equivalent plate length for an all-turbulent boundary layer with the same momentum thickness at the trailing edge as at the actual boundary layer.

(c) Calculate the coefficient of skin-friction drag per unit breadth for that part of the plate with

• A laminar boundary layer

• A turbulent boundary layer (Use the formulas based on the one-seventh-power-law velocity pro- file.) (d) Calculate the total drag per unit breadth.

(e) Estimate the percentage of drag due to the turbulent boundary layer alone

Reference no: EM131515298

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