1. For a turbulent boundary layer velocity profile given by u/Ue = (y/δ)1/9 , where Ue is the freestream velocity and δ is the boundary layer thickness, calculate the displacement thickness, the momentum thickness, and the shape factor. 2. A flat plate 1 m long and 0.5 m wide is parallel to a flow of air at a temperature of 25°C. The velocity of the air far from the plate is 20 m/s. (a) Is the flow laminar or turbulent? (b) Find the maximum thickness of the boundary layer. (c) Find the overall drag coefficient CF , assuming that transition occurs at the leading edge. (d) Find the total drag of the plate if the air covers both sides.

Structural Analysis
6th Edition
ISBN:9781337630931
Author:KASSIMALI, Aslam.
Publisher:KASSIMALI, Aslam.
Chapter2: Loads On Structures
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1. For a turbulent boundary layer velocity profile given by u/Ue = (y/δ)1/9 , where Ue is the freestream velocity and δ is the boundary layer thickness, calculate the displacement thickness, the momentum thickness, and the shape factor.

2. A flat plate 1 m long and 0.5 m wide is parallel to a flow of air at a temperature of 25°C. The velocity of the air far from the plate is 20 m/s.

(a) Is the flow laminar or turbulent?

(b) Find the maximum thickness of the boundary layer.

(c) Find the overall drag coefficient CF , assuming that transition occurs at the leading edge.

(d) Find the total drag of the plate if the air covers both sides.

 

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