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2. You are working for a glider manufacturer and have been asked to analyse the laminar boundary layer at a certain point on the smooth wing. The velocity profile at this point, u(y), is given by: น Us 2 3 = = 3 (²) ² − 2 (²) ³ + 4 (²5) + - A +B where 8 is the boundary-layer thickness and us is the velocity at the edge of the boundary layer. A and B are constants.

2. You are working for a glider manufacturer and have been asked to analyse the laminar boundary layer at a certain point on the smooth wing. The velocity profile at this point, u(y), is given by: น Us 2 3 = = 3 (²) ² − 2 (²) ³ + 4 (²5) + - A +B where 8 is the boundary-layer thickness and us is the velocity at the edge of the boundary layer. A and B are constants.

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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Please evaluate the shape factor and answer d)
2. You are working for a glider manufacturer and have been asked to analyse the laminar boundary layer at a certain point on the smooth wing. The velocity profile at this point, u(y), is given by: 3 ==3(²²-2 (²) + A (²) + B น Us where 8 is the boundary-layer thickness and us is the velocity at the edge of the boundary layer. A and B are constants.
Transcribed Image Text:2. You are working for a glider manufacturer and have been asked to analyse the laminar boundary layer at a certain point on the smooth wing. The velocity profile at this point, u(y), is given by: 3 ==3(²²-2 (²) + A (²) + B น Us where 8 is the boundary-layer thickness and us is the velocity at the edge of the boundary layer. A and B are constants.
d) Show that the pressure on the wing surface is increasing with downstream distance. Is this consistent with your calculations showing that the boundary layer is approaching separation? Explain your reasoning.
Transcribed Image Text:d) Show that the pressure on the wing surface is increasing with downstream distance. Is this consistent with your calculations showing that the boundary layer is approaching separation? Explain your reasoning.
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