a ull zain 1QK/sاسئله من 5 إلى 7. . .•.Q5| The velocity distribution for flow over a plate is gives by u = 2y – y where u isthe velocity in m/s at a distance y metres above the plate. Determine the velocity gradient and shearstress at the boundary and 1.5 m from it.Take dynamic viscosity of fluid as 0.9 N.s/m².Q6Two large fixed parallel planes are 12 mm apart. The space between the surfacesis filled with oil of viscosity 0.972 N.s/m². A flat thin plate 0.25 m² area moves through the oil at avelocity of 0.3 m/s. Calculate the drag force:(1) When the plate is equidistant from both the planes, and(ii) When the thin plate is at a distance of 4 mm from one of the plane surfaces.Q7. If the surface tension at air-water interfaceis 0.069 N/m, what is the pressure difference between inside andoutside of an air bubble of diameter 0.009 mm?

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Q5 |The velocity distribution for flow over a plate is gives by u = 2y – y where u is e velocity in m/s at a distance y metres above the plate. Determine the velocity gradient and shear ress at the boundary and 1.5 m from it. Take dynamic viscosity of fluid as 0.9 N.s/m².

Q5 |The velocity distribution for flow over a plate is gives by u = 2y – y where u is e velocity in m/s at a distance y metres above the plate. Determine the velocity gradient and shear ress at the boundary and 1.5 m from it. Take dynamic viscosity of fluid as 0.9 N.s/m².

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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