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If the energy of the incident photon is less than the work function:
A. An electron will be ejected
B. More than one electron will be ejected
C. An electron will not be ejected
D. Less than one electron will be ejected
C. An electron will not be ejected
For supersonic flow, the pressure of fluid must decrease as the fluid flow area of the duct.
A. Increases
B. Decreases
C. Remain the same
D. None of these
A. Increases
Density in term of viscosity is:
A. Kinematic viscosity / dynamic viscosity
B. Dynamic viscosity / kinematic viscosity
C. Kinematic viscosity x dynamic viscosity
D. None of the above
B. Dynamic viscosity / kinematic viscosity
Liquids and gases take the following characteristic(s) of their contents.
A. Volume
B. Shape
C. Shape and volume
D. Neither shape nor volume
B. Shape
Alcohol finds use in manometers as:
A. It provides a suitable meniscus for the inclined tube
B. Its density being less can provide longer length for a pressure difference, thus more accuracy can be obtained
C. A and B above are correct
D. Cheap and easily available
C. A and B above are correct
Which of the following statements about a Newtonian fluid is most accurate?
A. Shear stress is proportional to strain
B. Viscosity is zero
C. Shear stress is multi – valued
D. Shear stress is proportional to rate of strain
D. Shear stress is proportional to rate of strain
The normal stress is the same in all directions at a point in fluid:
A. Independent of the motion of one fluid layer relative to an adjacent layer
B. When there is no motion of one fluid layer relative to an adjacent layer
C. Only if the fluid is frictionless
D. Only if fluid is frictionless and incompressible
B. When there is no motion of one fluid layer relative to an adjacent layer
C. It is a shear stress
D. First slowly and then steeply
D. Biot number
D. all of the above
D. Thermal conductivity
D. All of the above
D. hysteresis
Which of the following can be used to measure the flow of water in a pipe of diameter 3000 mm?
A. Venturimeter
B. Rotameter
C. Nozzle
D. Pitot tube
D. Pilot tube
B. The sum of the individual pressures
D. All of the above conditions are together
C. At every point the velocity vector is identical in magnitude and direction for any given instant
D. States that energy is constant everywhere in the fluid
A. Kinetic energy and static pressure
A. 2.4m above the hydraulic gradient
A. The conservation of mass
C. Negligible
B. Boyle’s law
D. Low head axial flow turbine
A. The Darcy equation
B. The Darcy friction factor
C. Moody diagram
D. Vector difference of two velocities
A. 33 inch Hg
D. above the center of gravity
C. Below the centroid
D. Displaced volume of the fluid
D. The sum of pressure energy and potential energy
A. Total energy
A. Down in the direction of the flow
C. Velocity
A. Specific gravity liquids
A. Gravity, pressure and viscous
A. 4-5 m/s
D. In hydraulic structure with regulation provision
B. Less
C. Having partially full flow
C. Reynolds number and relative roughness
B. One-third of the total head supplied
In a nozzle if back pressure is same as inlet pressure then_.
A. No flow takes place
B. Maximum flow takes place
C. Flow becomes subsonic in diverging section
D. Flow becomes supersonic in converging as well as supersonic section
A. No flow takes place
D. Supersonic on one side and sub sonic on the other side
B. Principle of conservation of energy
A. It is a shear stress
D. Pressure
A. Kinetic energy and static pressure
B. Hydraulic radius
What is the coefficient of contraction?
A. The ratio of the area of vena contracta to the area of the orifice
B. The ration of actual discharge to the theoretical discharge
C. The ratio of the actual velocity to the theoretical velocity
D. The ratio of the effective head to the actual head
A. The ratio of the area of vena contracta to the area of the orifice
B. At a distance approximately ½ the diameter of the orifice
A. Fluid
The velocity of a fluid particle at the center of the pipe section is.
A. Maximum
B. Minimum
C. Average
D. Logarithmic average
A. Maximum
B. Decreases
D. It may occur owing to cohesion when the fluid is at rest
D. Half time
A. 10 times poise
B. Real or ideal
A. Kinetic viscosity
D. Experience of eddy current and turbulence
B. 100 kg/m3
A. Of no practical importance to designers
A. Atmospheric pressure
The volumetric change of the fluid caused by a resistance is called .
A. Volumetric strain
B. Volumetric index
C. Compressibility
D. Adhesion
C. Compressibility
C. Pressure
B. Cohesion
A. Less than the local speed of sound
D. Viscous and is in motion
C. The hydrostatic paradox
B. Conservation of energy equation
D. Is frictionless and incompressible
C. Barometric height relationship
B. Archimedes’ principle
D. Hysteresis losses
C. Froude’s number
C. None of the terms are interchangeable
A. A parabolic velocity profile
C. Pipe roughness
C. Conservation of mass
A. 4s/wd
B. Hydraulics
D. Pelton wheel
D. No load speed when governor mechanism fails
D. Kaplan turbine
C. Hydraulic diameter (the equivalent diameter)
B. The ratio of the area to the wetted perimeter
D. Air flowing supersonically
B. Empirical data
C. Nuclear energy
A. Has no velocity component tangent to it
D. Reduce the energy of flow
D. Dead storage
A. Down in the direction of the flow
A. Down in the direction of the flow
C. Hydrostatic pressure
A. The spatial derivative of velocity
B. Laminar flow