Applied Fluid Mechanics (7th Edition)
7th Edition
ISBN: 9780132558921
Author: Robert L. Mott, Joseph A. Untener
Publisher: PEARSON
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Chapter 17, Problem 17.2PP
As part of an advertising sign on the top of a tall building, a
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Chapter 17 Solutions
Applied Fluid Mechanics (7th Edition)
Ch. 17 - A cylinder 25 mm in diameter is placed...Ch. 17 - As part of an advertising sign on the top of a...Ch. 17 - Determine the terminal velocity (see Section 2.6.4...Ch. 17 - Calculate the moment at the base of a flagpole...Ch. 17 - A pitcher throws a baseball without spin with a...Ch. 17 - A parachute in the form of a hemispherical cup 1.5...Ch. 17 - Calculate the required diameter of a parachute in...Ch. 17 - A ship tows an instrument in the form of a 30...Ch. 17 - A highway sign is being designed to withstand...Ch. 17 - Assuming that a semitrailer behaves as a square...
Ch. 17 - A type of level indicator incorporates four...Ch. 17 - Prob. 17.12PPCh. 17 - A bulk liquid transport truck incorporates a...Ch. 17 - A wing on a race car is supported by two...Ch. 17 - Prob. 17.15PPCh. 17 - The four designs shown in Fig. 17.16 for the cross...Ch. 17 - Prob. 17.17PPCh. 17 - Prob. 17.18PPCh. 17 - An antenna in the shape of a cylindrical rod...Ch. 17 - Prob. 17.20PPCh. 17 - Prob. 17.21PPCh. 17 - Prob. 17.22PPCh. 17 - Assume that curve 2 in Fig. 17.5 is a true...Ch. 17 - Prob. 17.24PPCh. 17 - Prob. 17.25PPCh. 17 - A small, fast boat has a specific resistance ratio...Ch. 17 - Prob. 17.27PPCh. 17 - Assume that Fig. 17.11 shows the performance of...Ch. 17 - Calculate the total drag on an airfoil that has a...Ch. 17 - Prob. 17.30PPCh. 17 - Prob. 17.31PPCh. 17 - Prob. 17.32PPCh. 17 - Prob. 17.33PP
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- A cloud of coal particles is traveling through a system. The cloud diameter estimated to be 0.027 m and the individual particles are 50 um in diameter with the density of 1300 kg/m'. The total cloud is moving such that its drag coefficient is constant at 0.44. The individual particles in the cloud move much slower, such that the drag coefficient given by stock's law. The system has atmospheric air transporting and the cloud density is 190 kg/m3. Determine the ratio of internal velocity to cloud velocity. Atmospheric air density 1.2 kg/m'.arrow_forwardGiven the following measurements of mean winds and temperature from a 200-m mast in Netherlands on a September night: Table 1. Measurements of mean winds and temperature from a 200-m mast in Netherlands on a September night. Question: Determine the Richardson number (Ri) at heights of 7.5, 15, 30, 60, 100, 140, and 180 m (note: ∂Θ/∂z at height 7.5 m is the potential temperature gradient between 5 m and 10 m).arrow_forwardConsider an airplane flying at a pressure altitude of 11,650m and a density altitude of 11,780 m. Calculate the outside air temperaturearrow_forward
- The drag polar equation of a light airplane in clean configuration can be written as Cp = 0.358 + 0.0405 C₁². It has a weight of 18,681 N. The wing area is 14.41 m². Calculate the minimum power required in watts. (Round off answer with no decimal places, No units, No commas) Answer given: 1461792 A 5,000 lbs. aircraft has an excess power of 75 hp at sea level. If the service ceiling is 3,657.6 m, determine the time to climb from sea level to absolute ceiling in minutes. (Round off answer with no decimal places. No units, No commas) Answer given: 17arrow_forwardExample 3 The drag coefficient of a car increases when the sunroof is open, and it requires more aerodynamic drag. The car has a frontal area of 1.7 m2; and the C, values when the sunroof is closed and open are 0.32 and 0.41, respectively. If the car is moving at a constant velocity of 55 km/hr, determine the additional power consumption of the car when the sunroof is opened . Take the density of air to be 1.2 kg/m³. (a) if the air is calm, (b) if wind is blowing against the direction of the motion of the car at 30 km/hr, and (c) if wind is blowing in the same direction of motion of power to overcome the car at 50 km/hr.arrow_forwardWhat are the three main components of the standard atmosphere and which is most significant to aircraft performance? Describe the three main types of pressure in Aerodynamics?arrow_forward
- a smooth flat plate of length 5 m and width 2 m is moving with a velocity of 4 m/s in stationary air of density as 1.25 kg/m³ and kinematic viscosity 1.5 x 10-5 m²/s. determine thickness of the boundary layer at the trailing edge of the smooth plate. find the total drag on one side of the plate assuming that the boundary layer is turbulent from the very beginning.arrow_forwardWhen testing a new car, the car drives with a constant speed v = 140 km/h. Thepower of car’s engine is P = 120 kW and we know that 80% of this power is con-verted to movement. Determine the drag coefficient in air if the cross section of thecar has circular shape, its value is S = 3 m2, and air can be described as a liquidwith viscosity η = 2,2 · 10−3 Ns/m2 and density ρ = 1,2 kg/m3. Calculate theReynolds number and determine if the linear or quadratic drag equation is valid inthis case or neither of them.arrow_forwardfluid mechanics Question 3- The hot air balloon A hot air balloon is stationary about 3 m above the ground when a gust of wind suddenly arrives with a speed of 40 km/h. Determine the horizontal initial acceleration. The balloon is designed as a sphere with a diameter of 10 m. It is filled with 80°C air. Ambient air has a temperature of 10°C. The actual fabric balloon and basket with cargo has a mass of 200 kg.arrow_forward
- A stationary sphere in water moving at a velocity of 2.3 m/s experiences a drag of 6N.Another sphere three times the diameter is placed in a wind tunnel.The ratio of kinematic viscosities of air and water is 15, and the density of air is 1.28 kg/m3.Determine the velocity of the air and the drag which will give dynamically similar conditions.arrow_forwardFigure 2 shows a 0.25 kg kite with an area of 0.65 m² flies in a 25 km/h wind such that the weightless string makes an angle of 40° relative to the horizontal. The density of air is 1.22 kg/m3. If the pull on the string is 7 N, determine the lift and drag coefficient based on the kite area. Figure 2arrow_forward7. A flat plate has a length of 40 cm and width of 1 m. Air, at pressure of 2 atm,temperature of 57 C, and velocity of 3 m/s flows over the plate. Find the thicknessof the boundary layer at x = L.arrow_forward
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