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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: us 3 3³ (²) ² − ² (²) ²³ + +A ¹ (²5). + 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.

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: us 3 3³ (²) ² − ² (²) ²³ + +A ¹ (²5). + 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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Evaluate the boundary-layer shape factor, H.

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(²-2) + 4) + B A 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: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(²-2) + 4) + B A 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.
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