| a. 0.03 | ||
| b. 0.3 | ||
| c. 5 | ||
| d. 1 |
| a. 2,300-4,000 | ||
| b. 500-1,000 | ||
| c. 105 -106 | ||
| d. 50,000-100,000 |
| a. The friction factor decreases. | ||
| b. The friction factor is kept constant. | ||
| c. The friction factor increases. | ||
| d. None of the above |
| a. M L-1 | ||
| b. M L-1T-2 | ||
| c. M2L-1T | ||
| d. M-1T-2 |
| a. Thermal conductivity | ||
| b. Wind velocity | ||
| c. Atmospheric pressure | ||
| d. Relative humidity |
| a. The ratio of inertial forces to viscous forces. | ||
| b. The ratio of surface tension to inertial forces. | ||
| c. The ratio of inertial forces to gravitational forces. | ||
| d. The ratio of momentum diffusivity to thermal diffusivity. |
| a. The ratio of inertial forces ρV2/L to viscous forces μV/L2 | ||
| b. The ratio of surface tension to inertial forces | ||
| c. The ratio of gravitational force to fluid's inertia | ||
| d. The ratio of momentum diffusivity to thermal diffusivity |
| a. Movement of fluid slowly in layers in a pipe, without much mixing among the layers | ||
| b. A flow whose Reynolds number exceeds 2300 | ||
| c. Movements of fluid are chaotic with significant mixing | ||
| d. None of the above |
| a. Pressure is the force divided by the area over which the force is applied. | ||
| b. Pressure is equal to surface tension. | ||
| c. Pressure is the force times the area over which the force is applied. | ||
| d. Pressure is equal to the object's acceleration times its mass. |
| a. Reynolds number | ||
| b. Weber number | ||
| c. Prandtl number | ||
| d. Froude number |
| a. The locus of points of all the fluid particles that have passed through a given point | ||
| b. A family of curves, which are normal to the velocity vector of the flow | ||
| c. A family of curves that track the trajectories of fluid particles | ||
| d. A family of curves that are instantaneously tangent to the velocity vector of the flow |
| a. Pressure coefficient | ||
| b. Mach number M | ||
| c. Gas constant R | ||
| d. Friction factor f |
| a. V2/Lg | ||
| b. µ VL/ρ | ||
| c. VL/σ | ||
| d. None of the above |
| a. Streamlines cannot cross each other. | ||
| b. Streamlines provide a snapshot of the entire flow field. | ||
| c. Streamlines track trajectories of fluid particles. | ||
| d. The tangent at each point on a streamline is the direction of the velocity vector at that point. |
| a. The streamwise velocity component satisfies uz = 0. | ||
| b. "Boundary layers" from opposite sides of the pipe are separated and continue growing. | ||
| c. The radial component of the velocity is zero. | ||
| d. The entrance length depends on the Reynolds number. |
| a. Surface tension is responsible for the weight of liquid droplets. | ||
| b. Surface tension is measured in forces per unit length or of energy per unit area. | ||
| c. Surface tension is responsible for buoyancy. | ||
| d. None of the above |
| a. In the laminar zone, friction factor decreases as the Reynolds number increases. | ||
| b. In the turbulent zone, friction factor increases as the relative roughness (D/ε) increases. | ||
| c. Within the zone of complete turbulence, friction factor is independent of Reynolds number. | ||
| d. As relative roughness increases, the boundary of the complete turbulence zone shifts to the right. |
| a. Viscosity of a fluid depends strongly on its temperature. | ||
| b. Viscosity measures the friction between the fluid and the wall. | ||
| c. Shear stress is independent of viscosity. | ||
| d. For a given rate of angular deformation of a fluid, shear stress is inversely proportional to viscosity. |
| a. 15.7 kPa | ||
| b. 25.3 kPa | ||
| c. 3.21 kPa | ||
| d. 1.24 kPa |
| a. 1 m | ||
| b. 60 cm | ||
| c. 6 m | ||
| d. 20 cm |
| a. 331.3 m/s | ||
| b. 13.2 m/s | ||
| c. 1520.2 m/s | ||
| d. 212.5 m/s |
| a. 1.14 108 lbf | ||
| b. 4.14 108 lbf | ||
| c. 6.14 108 lbf | ||
| d. 9.14 108 lbf |
| a. 0.06 m3/s | ||
| b. 1.2 m3/s | ||
| c. 0.01 m3/s | ||
| d. 0.12 cm3/s |
| a. 3 | ||
| b. 5 | ||
| c. 12 | ||
| d. -2 |
| a. a = b | ||
| b. a = 2b | ||
| c. a = -b | ||
| d. a = -2b |
| a. -3 | ||
| b. 2 | ||
| c. 32 | ||
| d. -8 |
| a. Supersonic | ||
| b. Both turbulent and laminar | ||
| c. Turbulent | ||
| d. Laminar |
| a. 1.55 10-4 m2/s | ||
| b. 1.25 10-4 m2/s | ||
| c. 0.5 10-4 m2/s | ||
| d. 1.55 10-6 m2/s |
| a. 367 N/m2 | ||
| b. 65 N/m2 | ||
| c. 550 N/m2 | ||
| d. 107 N/m2 |
| a. 100 m/s | ||
| b. 400 m/s | ||
| c. 200 m/s | ||
| d. 50 m/s |
| a. 15 m | ||
| b. 50 m | ||
| c. 12 m | ||
| d. 8 m |
| a. 11 µ | ||
| b. 0 | ||
| c. µ | ||
| d. 2 µ |
| a. 62 µ | ||
| b. 0 | ||
| c. 22µ | ||
| d. 38 µ |
| a. µ | ||
| b. 10µ | ||
| c. 20πµ | ||
| d. 10πµ |
| a. 0.5 g | ||
| b. 2.6 g | ||
| c. 5.2 g | ||
| d. 7.9 g |
| a. 10 s | ||
| b. 12 s | ||
| c. 7 s | ||
| d. 20 s |
| a. 1.26 N | ||
| b. 5.23 N | ||
| c. 2.12 N | ||
| d. 0.12 N |
| a. 5 m/s | ||
| b. 1 m/s | ||
| c. 2 m/s | ||
| d. 0.5 m/s |
| a. 31.1 kN | ||
| b. 27.2 kN | ||
| c. 19.6 kN | ||
| d. 59.5 kN |
| a. 7.6 mm | ||
| b. 5.3 mm | ||
| c. 1.2 mm | ||
| d. 8.7 mm |
| a. 0.15 psi | ||
| b. 1.24 psi | ||
| c. 16.3 psi | ||
| d. 350 psi |
| a. 1.2 l/s | ||
| b. 3.9 l/s | ||
| c. 45.1 l/s | ||
| d. 0.2 l/s |
| a. 0.0004 | ||
| b. 0.004 | ||
| c. 0.04 | ||
| d. 0.4 |
| a. 119 Pa/m | ||
| b. 1049 Pa/m | ||
| c. 22 Pa/m | ||
| d. 11 Pa/m |
| a. 5.3 mPa s | ||
| b. 0.005 cP | ||
| c. 5.3 Pa s | ||
| d. 5.3 P |
| a. 0.3 atm | ||
| b. 0.03 atm | ||
| c. 3 Pa | ||
| d. 30 Pa |
| a. Mf D v/μ | ||
| b. Mf/(D μ) | ||
| c. Mf v ρ/μ | ||
| d. Mf ρ D/μ |
| a. 1.22 | ||
| b. 2.0 | ||
| c. 0.52 | ||
| d. 7 |
| a. 1 | ||
| b. 2 | ||
| c. 1.5 | ||
| d. 5 |
Use this expression to calculate the product τrz 2 π R
(where τrz = μ dv/dr) for a Newtonian fluid evaluated at the pipe wall. Which of the following expressions matches your result?
| a. dP/dz | ||
| b. 2 π R dP/dz | ||
| c. μ dP/dz | ||
| d. R2π dP/dz |
| a. 225 atm | ||
| b. 0.225 atm | ||
| c. 2250 Pa | ||
| d. 225 Pa |
| a. 0.2 Pa s | ||
| b. 1 cP | ||
| c. 0.2 cP | ||
| d. 1 Pa s |
| a. 112 | ||
| b. 225 | ||
| c. 325 | ||
| d. 176 |
| a. 40 | ||
| b. 33 | ||
| c. 32 | ||
| d. 35 |
| a. 280, 10 | ||
| b. 210, 10 | ||
| c. 280, 20 | ||
| d. 210, 20 |