Concept explainers
The error involved in the given case.
Answer to Problem 109P
The error involved between experimental and Stokes law is
Explanation of Solution
Given information:
Concept used:
Calculation:
Hence, the Stokes law is valid.
Now let us calculate the error for the aluminium ball of 4 mm diameter.
Concept used
Calculation:
Hence, the Stokes law is valid.
The error involved between experimental and Stokes law is
Now let us calculate the error for the aluminium ball of 10 mm diameter.
Concept used:
Calculation:
Hence, the Stokes law is valid.
The error involved between experimental and Stokes law is
Conclusion:
The error involved between experimental and Stokes law is
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Chapter 11 Solutions
Fluid Mechanics: Fundamentals and Applications
- A long circular cylinder rotates at a constant angular velocity of 100 rad/s while subjected to a uniform cross flow of air at a velocity of 15 m/s as shown. If the density of the air is 1.20 kg/m², find the lift per unit length of cylinder. y U= 15 m/s @ = 100 rad/s R = 0.25 m airarrow_forwardWater travels through a circular pipe with a diameter of 400 mm and at a speed of 5 m/s. The inertial force created by the flow is:Question 15Answera.10000 kgs/mb.100000 kgs/mc.1000 kgs/md.1000000 kgs/marrow_forwardPRACTICE II Use the worked example above to help you solve this problem. A rocket has a total mass of 1.04 x 105 kg and a burnout mass of 1.07 x 104 kg, including engines, shell and payload. The rocket blasts off from Earth and exhausts all its fuel in 3.86 min, burning the fuel at a steady rate with an exhaust velocity of ve = 4.16 x 10³ m/s. (a) If air friction and gravity are neglected, what is the speed of the rocket at burnout? m/s (b) What thrust does the engine develop at liftoff? N (c) What is the initial acceleration of the rocket if gravity is not neglected? m/s² (d) Estimate the speed at burnout if gravity isn't neglected. m/s EXERCISE A spaceship with a mass of 4.90 x 104 kg is traveling at 5.71 x 10³ m/s relative to a space station. What mass will the ship have after it fires its engines in order to reach a speed of 8.16 x 10³ m/s? Assume an exhaust velocity of 4.73 x 10³ m/s. kg HINTS: GETTING STARTED I I'M STUCK!arrow_forward
- Consider the propeller tube shown in. The density of air is Pa = 1 23 kg/m. The diameter of the nozzles at B, C, D, and E is 100 mm 100 mm 0.5 m M D 60 rad/s 0.5 m 0.5 m 0.5 m Part A If the propeller tube rotates at a constant rate of 60 rad/s when 1.80 kg/s of air enters at A, determine the frictional torque M acting on the tube. Express your answer to three significant figures and include the appropriate units. Enter positive value if the moment is counterclockwise and negative value if the moment is clockwise.arrow_forwardA wind turbine with an extraction ratio (torque power/drag power) of 1.34 rotates at 0.39 rad/s in a wind with velocity 20m/s. The disc area is 339 sq m and the torque generated is 817 kNm. Taking air density as 1.29 kg/m/m/m, calculate the advance angle at the blade tip, assuming flow arrives at the disc axially. Express your answer in degrees.arrow_forwardA semi-cylindrical concrete structure having a radius of 3 m and length of 5 m is rested on ground. Wind (air having a density ρ=1,2 kg/m3 ) at a free-sream speed of 10 m/s with an atmospheric pressure of 100 kPa far upstream the structure blows over the structure. The air entrance to the structure is at ground level corresponding to the forward stagnation point and the magnitude of minimum pressure is acting on the top of the structure a lift force is generated. Estimate the lift coefficient C L =? with calculated magnitude of lift force from potential flow theoryarrow_forward
- Do fastarrow_forward6m A cannonball with an initial height of 1.00 meter above the ground is fired from a cannon at an angle Vo of 53° above the horizontal. The cannonball 70 m travels a horizontal distance of 90 meters to a 70 meter high castle wall, and passes over 6 meters above the highest point of the wall. (Assume air friction is negligible.) 90 m (Take g=10m/s², sin53°=cos37°=0,8, sin37°=cos53°=0,6). Determine how much time it takes for the ball to reach the wall.arrow_forwardA horizontal fan (such as that shown in example 5.24) pulls in stagnant air (ie. basically stationary air) atatmospheric pressure; the air approaches the fan outlet with speed 44 ft/sec (ie. 30 mph) and with static pressure 0.3 psi. The air flowing through the fan can be assumed to have a constant density of 2.4*10-3 slug/ft3. The air losses due to friction are 0.1 psi (or 6000 ft-lb/slug of air passing from the fan inlet to the outlet). a) Determine the shaft work in ft-lb/slug b) If the fan outlet area is 2 ft2, determine the rate of work on the air.arrow_forward
- A block of mass m slides on a horizontal rough surface head on into a spring of spring constant k = 730 N/m, as shown in Figure. When the block is x = 0.8 meter away from the spring, it has a velocity v = 4.33 m/s. When the block stops, it has compressed the spring by 6.5 cm. The coefficient of kinetic friction between the block and the surface is 0.1. What is the block's mass m (in kg)? Provide your answer with 2 decimal places. Take g = 9.81 m/s2 Varrow_forward3. A semi-cylindrical concrete structure having a radius of 5 m and length of 3 m is rested on ground. Wind (air having a density p=1,2 kg/m3 ) at a free-sream speed of 3 m/s with an atmospheric pressure of 100 kPa far upstream the structure blows over the structure. The air entrance to the structure is at ground level corresponding to the forward stagnation point and the magnitude of minimum pressure is acting on the top of the structure a lift force is generated. Estimate the lift coefficient CL =? with calculated magnitude of lift force from potential flow theory Lütfen birini seçin: а. 2 b. 3 С. 1 d. 12 е. 4arrow_forwardA two-dimensional diverging duct is being designed to diffuse the high-speed air exiting a wind tunnel. The x-axis is the centerline of the duct (it is symmetric about the x-axis), and the top and bottom walls are to be curved in such a way that the axial wind speed u decreases approximately linearly from u1 = 300 m/s at section 1 to u2 = 100 m/s at section 2 . Meanwhile, the air density ? is to increase approximately linearly from ?1 = 0.85 kg/m3 at section 1 to ?2 = 1.2 kg/m3 at section 2. The diverging duct is 2.0 m long and is 1.60 m high at section 1 (only the upper half is sketched in Fig. P9–36; the halfheight at section 1 is 0.80 m). (a) Predict the y-component of velocity, ?(x, y), in the duct. (b) Plot the approximate shape of the duct, ignoring friction on the walls. (c) What should be the half-height of the duct at section 2?arrow_forward
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