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Incompressible laminar B. L flow growing along the surface of a flat plate, of chord c. The B. L Upper Boundar of the CV thickness is given by 8/c = 5//Re, and the skin friction is C = D'/9ooc = 1.328//Rec, where the Reynolds number Re. = P.VC/Hoo. The velocity profile is assumed by u/V. =(y/8)". Calculate the value of n consistent with the information above U1 Vo. Velocity profile e of boundary layer

Incompressible laminar B. L flow growing along the surface of a flat plate, of chord c. The B. L Upper Boundar of the CV thickness is given by 8/c = 5//Re, and the skin friction is C = D'/9ooc = 1.328//Rec, where the Reynolds number Re. = P.VC/Hoo. The velocity profile is assumed by u/V. =(y/8)". Calculate the value of n consistent with the information above U1 Vo. Velocity profile e of boundary layer

Structural Analysis
Structural Analysis
6th Edition
ISBN:9781337630931
Author:KASSIMALI, Aslam.
Publisher:KASSIMALI, Aslam.
Chapter2: Loads On Structures
Section: Chapter Questions
Problem 1P
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Incompressible laminar B. L flow growing along the surface of a flat plate, of chord c. The B. L Upper boundary of the CV thickness is given by 8/c = 5//Re, and the skin u, friction is C = D'/qC = 1.328//Rec, where the Reynolds number Re. = PVoC/Hoo. The velocity profile is assumed by u/V =(9/8)". Calculate the value of n consistent with the information above Voo %3D %3D Velocity -profile %3D Edge of boundary layer
Transcribed Image Text:Incompressible laminar B. L flow growing along the surface of a flat plate, of chord c. The B. L Upper boundary of the CV thickness is given by 8/c = 5//Re, and the skin u, friction is C = D'/qC = 1.328//Rec, where the Reynolds number Re. = PVoC/Hoo. The velocity profile is assumed by u/V =(9/8)". Calculate the value of n consistent with the information above Voo %3D %3D Velocity -profile %3D Edge of boundary layer
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