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55.

The shear stress distribution for a fluid flowing in between the parallel plates, both at rest, is                        


A. constant over the cross section B. parabolic distribution across the section
C. zero at the mid plane and varies linearly with distance from mid plane D. zero at plates and increases linearly to midpoint




56.

If x is the distance from leading edge, then the boundary layer thickness in laminar flow varies as                        


A. x B. x
C. x D. x/7




57.

Stanton diagram is a                        


A. log-log plot of friction factor against Reynolds number B. log-log plot of relative roughness against Reynolds number
C. semi-log plot of friction factor against Reynolds number D. semi-log plot of friction factor against relative roughness




58.

The depth 'd' below the free surface at which the point velocity is equal to the average velocity of flow for a uniform laminar flow with a free surface, will be
where D is the depth of flow.                        


A. 0.423 D B. 0.577 D
C. 0.223 D D. 0.707 D




59.

The boundary layer thickness in turbulent flow varies as
where x is the distance from leading edge.                        


A. x"7 B. x,/2
C. x4/5 D. x3/5




60.

The distance y from pipe boundary, at which the point velocity is equal to average velocity for turbulent flow, is
where R is radius of pipe.                        


A. 0.223 R B. 0.423 R
C. 0.577 R D. 0.707 R




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