A. 90 m/sec
B. 22.5 m/sec
D. 33 m/sec
A. Coefficient of contraction of a venturimeter is unity
B. Discharge is independent of orientation of venturimeter whether it is horizontal, vertical or inclined
C. Flow nozzle is cheaper than venturimeter but has higher energy loss
B. between 1.5 d and 2d
C. greater than 2d
D. between d and 1.5 d
A. 600
B. 337.5
C. 300
B. 8 km
C. 20 km
D. 4 km
A. 10%
B. 15%
C. 20%
A. weight of liquid vertically above the curved surface
C. force on the horizontal projection of the curved surface
D. product of pressure intensity at its centroid and area
B. 2
C. 2-Mar
D. 3-Feb
A. 27/8
B. 3-Apr
D. 2-Mar
A. equal to atmospheric
B. more than atmospheric
C. none of the above
A. pressure intensity of liquid
C. pressure intensity of gas
D. discharge
A. 0.25
D. 0.5
A. non-uniform flow</strong>
B. correct answer is?
C. unsteady flow
D. uniform flow
A. 0.7H
C. 0.611
D. 0.855
A. unsteady flow
B. uniform flow
C. correct answer is?
E. non-uniform flow</strong>
A. none of the above
C. momentum
D. energy
B. Upper critical Reynolds number is the number at which turbulent flow changes to laminar flow
C. Lower critical Reynolds number has the value 2000 in pipe flow
D. Upper critical Reynolds number is significant in pipe flow problems.
A. maximum at the pipe wall
B. none of the above
D. independent of shear stress
A. semi-log plot of friction factor against Reynolds number
B. semi-log plot of friction factor against relative roughness
C. log-log plot of relative roughness against Reynolds number
B. 0.10 cm
C. 0.40 cm
D. 0.05 cm
A. 0.577 R
C. 0.423 R
D. 0.707 R
B. the viscosity of fluid
C. the length of pipe
D. the original head
A. a sphere
C. a circular disc or plate held normal to flow
D. a cylinder
A. 0.1
C. 0.0001
D. 0.001
B. a trial solution is not necessary
C. the head loss is same through each pipe
D. the discharge through each pipe is added to obtain total discharge
A. pressure
C. kinematic viscosity
D. surface tension
B. one which obeys Newtons law of viscosity
C. very viscous
D. frictionless and compressible
A. float
B. rise until its weight equals the buoyant force
B. is independent of pressure for very high pressure intensities
C. decreases with increase in temperature
D. is independent of temperature
B. H/3
C. H/2
D. 2 H/5
A. inversely as the square of the radial distance
C. inversely as the radial distance
D. linearly with radial distance
A. dyne-sec/cm2
C. gm/cm2-sec
D. gm/cm-sec2
A. 15 kN
B. 5kN
D. 20 kN
C. is independent of Reynolds number
D. decreases with higher Reynolds number
A. lowest pressure intensity occurs at rear stagnation point
C. lowest pressure intensity occurs at front stagnation point
D. highest intensity of pressure occurs around the circumference at right angles to flow
B. free vortex at center and forced vortex outside
C. free vortex motion
D. forced vortex motion
A. always above the centroid of the area
D. at the centroid of the submerged area
A. 2/3 R
C. 1/2 R
D. 3/4R
B. a cylinder
C. a streamlined body
D. a sphere
B. 3.75 m
C. 4.5m
D. 4.0 m
A. the bubble will move to the front
B. the bubble will move to the rear </strong>
D. d out which of the above statements are correct ?
E. the ball will move to the rear
B. a function of temperature only
C. independent of the flow
D. a physical property of the fluid.
A. 0.223 D
B. 0.707 D
C. 0.423 D
A. directly proportional to the square of its radial distance from the axis of rotation
B. inversely proportional to its radial distance from the axis of rotation
C. inversely proportional to the square of its radial distance from the axis of rotation
A. is independent of coordinates
B. is never zero
D. is always zero
A. 10 kN/m2
B. 12 kN/m2
C. 4 kN/m2
B. velocity at stagnation point
C. dynamic pressure
D. static pressure
A. x,/2
B. x7
D. x3/5
A. from reservoir A to reservoirs B and C
C. from reservoir B to reservoirs C and A
D. unpredictable
B. g/3
C. g/2
D. 2g/3
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