B. FLT, ML-1T-1
C. F-1L2T-1, MLT-3
D. ML-1T-3, F-1L2T
A. Data insufficient, cannot be predicted
B. Less than
C. Same as
B. Shear stress over the cross-section is proportional to the distance from the surface of the pipe
C. ume of circumscribing cylinder</strong>
D. Velocity profile varies hyperbolically and the shear stress remains constant over the crosssection
E. Average flow occurs at a radial distance of 0.5 r from the centre of the pipe (r = pipe radius)
A. Chromium
B. Aluminium
D. Copper
A. 100
C. 320
D. 160
A. 700
C. 630
D. 7000
A. Equal to
C. Less than
D. Either A. or B.
A. 1.5
C. 5
D. 0
A. Steady, compressible, irrotational
B. Unsteady, incompressible, irrotational
D. Steady, compressible and along a streamline
B. Tee
C. Reducer
D. Elbow
A. Sum of the fluid friction and pressure forces is equal and opposite to gravity forces
C. Fluid friction is zero
D. Pressure forces equal gravity forces
A. Turbulent
C. Rotational
D. Unsteady
A. 0.35 0.55
B. 0.75 0.90
C. 0.5 0.75
A. Gravity
C. Viscous
D. None of these
A. Co-efficient of contraction only
B. Its orientation
C. None of these
A. Constant
B. Independent of time
D. Neither A. nor B.
A. Head loss and velocity
B. Velocity and relative roughness
D. Reynolds number and friction factor
A. Density
C. Viscosity
A. None of these
B. At rest and when the frictionless fluid is in motion
C. Frictionless and at rest
A. Thixotropic
B. Rheopectic
A. h2 < h1 < h3
B. h1 < h2 < h3
D. h1 > h2 > h3
A. Euler
C. Weber
D. Mach
A. Tall narrow vessel
B. Deep bed of solids
C. Very large particles
A. Radius of
B. Fluid velocity leaving
C. Speed of
A. Greatly affected by moderate changes in pressure
B. Greatly affected only by moderate changes in temperature
D. Sensible to changes in both temperature & pressure
A. H3/2
B. H1/2
D. H2/3
A. 12
B. 8
C. 20
B. Fluid momentum is constant
D. Rate of mass outflow is equal to the rate of mass inflow
A. (d1/d2)0.8
B. d1/d2
C. (d1/d2)2
B. static
D. Dynamic
A. Hyperbolic
B. Linear
D. Parabolic
B. Independent of
C. Inversely proportional to the square root of
D. Directly proportional to
C. Colebrook formula
D. Fanning equation
B. Blower
C. Centrifugal pump
D. Centrifugal fan
A. Irrotational flow only
B. None of these
D. Ideal/non i viscous fluids only
A. Increases the volumetric efficiency of the pump
B. Smoothens the flow by avoiding pulsations
C. Saves the pump from the danger of cavitation
A. Mass
B. Energy
C. Both A. & B.
A. Expansion of flow after sudden contraction
D. Boundary friction
A. Pressure pipeline
B. Tunnel
C. Penstock
A. Depends mainly on cross-sectional shape
C. Is primarily a friction drag
D. Is independent of body length
A. Less than
C. Equal to
D. Either more or less than
A. Develops noise
C. Increase in thrust
D. Decrease in effect
A. Turbulence in flow
C. Steep slope in flow
D. Unsteady nature of flow
A. Incomplete priming
C. Low available NPSH and air leaks in the suction pipe
D. Too high a suction lift
A. Weir
B. Cup and vane anemometer
B. Inside diameter
D. Thickness
A. MLT
B. ML-1T
D. MLT-1
A. Minimum velocity of fluid stream
D. More diameter compared to orifice diameter
B. < 1
C. 1
A. Data insufficient to predict
C. More power than
D. Same power as
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