A fan that can provide air speeds up to 50 m/s is to be used in a low-speed wind tunnel with atmospheric air at
Want to see the full answer?
Check out a sample textbook solutionChapter 6 Solutions
Fundamentals of Heat and Mass Transfer
Additional Engineering Textbook Solutions
Thinking Like an Engineer: An Active Learning Approach (3rd Edition)
Fox and McDonald's Introduction to Fluid Mechanics
INTERNATIONAL EDITION---Engineering Mechanics: Statics, 14th edition (SI unit)
Engineering Mechanics: Statics & Dynamics (14th Edition)
Engineering Mechanics: Dynamics (14th Edition)
Introduction To Finite Element Analysis And Design
- Air at 1000C flows at an inlet velocity of 2 m/s between two parallel flat plates spaced 1 cm apart. Estimate the distance from the entrance to the point where the boundary layers meet.arrow_forwardI need correctlyarrow_forward1. Consider a new wind tunnel to test and utilise the effects of boundary layer conditions in order to maintain the velocity of a fluid. Laminar airflow enters a square duct design through a 0.25m² opening, as is shown in Figure 1. Because the boundary layer displacement thickness increases in the direction of flow, it is necessary to increase the cross-sectional size of the duct if a constant U=1 m/s velocity to be maintained outside the boundary layer. Assume standard air temperature in the calculation. U = 1 m/s 0.25 m2 d(x) 1 m/s Figure 1 a) Determine the expression of the duct size, d, in consideration to maintain the velocity outside the boundary layer. b) Plot a graph of the duct size, d, as a function of x for 0arrow_forwardA series of 10 chips are placed on an insulating substrate as shown in the figure. Each chip has a length (Lc) of 15 mm, it is 20 mm wide and 10 mm thick. Upstream of the chips there is an input length (Le) of 15 mm. Whether each chip should dissipate 0.5 W and stay at a maximum temperature of 80 °C, what should be the speed uꝏ that the ambient air at 25 °C should be blown so that this condition is met? The emissivity of the chips is 0.8. consider that the chips do not exchange heat with each other and there is a turbulence generator upstream of the plate.arrow_forwardFind the related Average Nusselt number equationarrow_forwardi need the answer quicklyarrow_forwardAir at free-stream velocity of 9 m/s flows over a thin flat plate of length 3 m and width 1.5 m. A laminar boundary layer develops from the leading edge of the flat plate. At Re. = 500 000, the boundary layer becomes a turbulent boundary layer where x is the distance from the leading edge. Pair = 1.2 kg/m², µair = 1.8 x 10$ kg/m.s (a) Estimate the length of the laminar boundary layer. (b) Estimate the drag force due the laminar boundary layer on one side of the flat plate. (c) Estimate the boundary layer thickness and wall shear stress at x = 2.5 m.arrow_forward(b) Air at 25 °C flows past a flat plate at 1.5 m/s. The plate measures 500 mm (length) x 200 mm (breadth) and is maintained at a uniform temperature at 85 "C. Calculate the heat loss from the plate, if the air flows parallel to the plate. Pr = 0.796 y = 1897 x 106 m²/s k = 0.03896 W/m K 0.5 Nu L = 0.332Re, pr0.333arrow_forwardShow every step please not Ai generated im trying to understand what im doing wrong.arrow_forwardAir flows at 15°C with a velocity of 12 m/s over a flat plate whose length is 80 cm. Using one-seventh power law of the turbulent flow, what is the boundary layer thickness at the end of the plate? (The kinematic viscosity of air is 1.470 × 10−5 m2/s.) (a) 1.54 cm (b) 1.89 cm (c) 2.16 cm (d ) 2.45 cm (e) 2.82 cmarrow_forwardanswer quicklyarrow_forwardQ4-Q6: A device is used to cool hot copper spheres of diameter 5 mm from an average temperature of 200C to 50C by letting them fall in air at 25°C and latm. Use drag coefficient C, = 0.4 and Whitaker correlation in your calculations. Assume the spheres fall at their terminal velocities during the process. Q4 improve the accuracy? Iteration is not required. ) Determine the terminal velocity of a sphere. Is the use of C, = 0.4 appropriate? If not, how toarrow_forwardarrow_back_iosSEE MORE QUESTIONSarrow_forward_ios
- Principles of Heat Transfer (Activate Learning wi...Mechanical EngineeringISBN:9781305387102Author:Kreith, Frank; Manglik, Raj M.Publisher:Cengage Learning