B. None of these

C. Does not depend on Mach number

D. Cannot drop and then increase again downstream

A. None of these

B. Froude number

C. Pressure co-efficient

B. m/N. sec

C. N/m2

D. m2 /sec

A. H2/3

C. H3/2

D. H1/2

A. Are directly coupled

C. Have the same diameter

D. None of these

B. Expanding tube at increasing rate

C. Long pipe at constant rate

D. Expanding tube at constant rate

A. Mass

B. Energy

C. Both A. & B.

A. Be quadrupled

B. Decrease

D. Remain same

A. Turbulence in flow

B. Steep slope in flow

D. Unsteady nature of flow

A. More diameter compared to orifice diameter

B. None of these

C. Minimum velocity of fluid stream

A. Unsteady uniform

C. Steady uniform

D. Unsteady non-uniform

A. Vacuum as well as the atmospheric

C. Gage

D. Absolute

B. 4d

C. d

D. 2d

A. None of the above

C. Drag force and gravitational forces are important

D. Inertial and drag forces are important

B. Gravity forces

C. Viscous forces

D. Pressure forces

A. Mach number

C. Prandtl number

D. Weber number

A. 2

B. 2.828

D. 4

A. Constant

B. Independent of time

D. Neither A. nor B.

A. Steady uniform

B. Non-steady uniform

D. Steady non-uniform

A. Measuring small pressure difference in liquids

C. Measuring the difference of the impact & the static pressure

D. Measuring small pressure difference in gases

A. 0.001

C. 0.1

D. 1

B. Is zero irrespective of the Reynolds number

C. None of these

D. Is not a function of Reynolds number

A. Independent of

C. Inversely proportional to the square root of

D. Directly proportional to

B. 0.93 to 0.98

C. 0.2 to 0.3

D. 0.02 to 0.03

A. None of these

B. Decreases as V2

C. Decreases linearly with V

A. 0

C. < 1

D. 1

A. Submerged weight

C. Own volume

D. Submerged volume

A. Force exerted

B. Power developed

C. Work done

A. Union

B. Elbow

C. None of these

A. ?/?s = 0

B. ?/?s = constant

D. ?/?t = constant

A. Pipe diameter

C. Type of orifice & the Reynolds number

D. Ratio of pipe diameter to orifice diameter

A. >25

C. 2 to 5

D. 15 to 25

A. Re <> 1, accelerating flow

C. Re << 1, decelerating flow

A. Minimising wall friction

B. Suppressing boundary layer separation

D. Neither A. nor B.

A. Velocity and relative roughness

C. Head loss and velocity

D. Reynolds number and friction factor

B. Tall narrow vessel

C. Very large particles

D. Deep bed of solids

A. Depends mainly on cross-sectional shape

B. Is primarily a friction drag

D. Is independent of body length

A. Centrifugal pump

B. Centrifugal fan

D. Blower

A. F-1. L

B. F.L-2

C. F-2. L

A. 0.5

B. 1

D. -0.5

A. Static pressure

C. Dynamic pressure

D. Point velocity

B. pitot tube

C. Venturimeter

D. Orificemeter

A. Less than

B. Data insufficient, cannot be predicted

D. Same as

A. Reynolds

B. Blake-Plummer

C. Pascal

A. Convert velocity head to pressure head

B. Reduce the discharge fluctuation

D. Convert pressure head to velocity head

B. 4000

C. 3000

D. 1500

A. Fluid-particle interaction

B. Psychrometry

C. Power consumption in agitated vessels

A. Increase the mass flow rate of fluid

C. None of these

D. Develop effective pressure rise by the pump

B. Sluggish

C. Boiling

D. Teeter

A. The line connecting the mid-points of flow cross-sections

B. Always the path of a particle

C. Defined for uniform flow only