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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.

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.

Elements Of Electromagnetics
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
Problem 1.1MA
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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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