A. 300
B. 337.5
C. 600
D. 675
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Related Mcqs:
- If the dynamic viscosity of a fluid is 0.5 poise and specific gravity is 0.5, then the kinematic viscosity of that fluid in stokes is__________________?
- A. 0.25 B. 0.50 C. 1.0 D. none of the above...
- If a sphere of diameter 1 cm falls in castor oil of kinematic viscosity 10 stokes, with a terminal velocity of 1.5 cm/sec, the coefficient of drag on the sphere is________________?
- A. less than 1 B. between 1 and 100 C. 160 D. 200...
- A valve is suddenly closed in a water main in wl.ich the velocity is 1 m/sec and velocity of pressure wave is 981 m/ sec. The inertia head at the valve will be________________?
- A. 1 m B. 10m C. 100m D. none of the above...
- The depth ādā 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_________________?
- A. 0.423 D B. 0.577 D C. 0.223 D D. 0.707 D where D is the depth of flow...
- A fluid of kinematic viscosity 0.4 cm2/sec flows through a 8 cm diameter pipe. The maximum velocity for laminar flow will be__________________?
- A. less than 1 m/sec B. 1 m/sec C. 1.5 m/sec D. 2 m/sec...
- The discharge of a liquid of kinematic viscosity 4 cm2/sec through a 8 cm dia-meter pipe is 3200n cm7sec. The type of flow expected is__________________?
- A. laminar flow B. transition flow C. turbulent flow D. not predictable from the given data...
- In a two dimensional incompressible steady flow around an airfoil, the stream lines are 2 cm apart at a great distance from the airfoil, where the velocity is 30 m/sec. The velocity near the airfoil, where the stream lines are 1.5 cm apart, is_________________?
- A. 22.5 m/sec B. 33 m/sec C. 40 m/sec D. 90 m/sec...
- The boundary layer thickness at a distance of l m from the leading edge of a flat plate, kept at zero angle of incidence to the flow direction, is O.l cm. The velocity outside the boundary layer is 25 ml sec. The boundary layer thickness at a distance of 4 m is__________________?
- A. 0.40 cm B. 0.20 cm C. 0.10 cm D. 0.05 cm Assume that boundary layer is entirely laminar...
- If velocity is zero over l/3rd of a cross-section and is uniform over remaining 2/3rd of the cross-section, then the correction factor for kinetic energy is__________________?
- A. 4/3 B. 3/2 C. 9/4 D. 27/8...
- When the velocity distribution is uniform over the cross-section, the correction factor for momentum is__________________?
- A. 0 B. 1 C. 4/3 D. 2...
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