Consider a flat plate that is L = 3 m long and of unit width immersed in a free stream flow of air with velocity 11 m/s. Assume the surface is smooth and the boundary layer is turbulent from the leading edge. Use flat-plate boundary layer theory to: a. Calculate the drag force on the plate (consider only one side.) b. Calculate the contribution of the skin friction drag on the section 2 m < x < 2.5 m to the total drag force.

Principles of Heat Transfer (Activate Learning with these NEW titles from Engineering!)
8th Edition
ISBN:9781305387102
Author:Kreith, Frank; Manglik, Raj M.
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Chapter5: Analysis Of Convection Heat Transfer
Section: Chapter Questions
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Consider a flat plate that is L = 3 m long and of unit width immersed in a
free stream flow of air with velocity 11 m/s. Assume the surface is smooth and the
boundary layer is turbulent from the leading edge. Use flat-plate boundary layer
theory to:
a. Calculate the drag force on the plate (consider only one side.)
b. Calculate the contribution of the skin friction drag on the section 2 m < x <
2.5 m to the total drag force.
Transcribed Image Text:Consider a flat plate that is L = 3 m long and of unit width immersed in a free stream flow of air with velocity 11 m/s. Assume the surface is smooth and the boundary layer is turbulent from the leading edge. Use flat-plate boundary layer theory to: a. Calculate the drag force on the plate (consider only one side.) b. Calculate the contribution of the skin friction drag on the section 2 m < x < 2.5 m to the total drag force.
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