Air at 47 ° C and 1 atm flows over a flat plate at 40 m/s. The plate is 90 cm long
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Q: w. Why? Elabo
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Q: A 20degC water flows to 50cmx60cm flat plate with velocity of 6m/s . The flat plate surface…
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Q: Air at 20°C, 1 atm flows with a velocity of 4.5 m/s over a flat plate having a sharp leading edge.…
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Q: Atmospheric air with free flow velocity U_∞= 30 m/s flows through a circular cylinder at T_∞= 250 K…
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- 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.5.6 A fluid flows at 5 over a wide, flat plate 15 cm long. For each from the following list, calculate the Reynolds number at the downstream end of the plate. Indicate whether the flow at that point is laminar, transition, or turbulent. Assume all fluids are at 40°C. (a) air, (b) , (c) water, (d) engine oil.A gas at 20°C and 1 atm flow at 6 ft/s past a thin flat plate.At x = 3 ft, the boundary layer thickness is 0.052 ft.Assuming laminar flow, which of the gases in Table A.4 isthis likely to be?
- An ideal gas, at 20°C and 1 atm, flows at 12 m/s past a thinflat plate. At a position 60 cm downstream of the leadingedge, the boundary layer thickness is 5 mm. Which of the13 gases in Table A.4 is this likely to be?The air at 65°C and with a viscosity of 1.86x10^-5 m^2/s flows along a flat plate at 12 m/s, under laminar regime, which distance, from the leading edge, where the boundary layer thickness reaches 0.5 cm?Consider the laminar boundary layer flow of an isothermal fluid ( U ∞ , T ∞ ) over a flat isothermal wall ( T 0 ). At a certain distance x from the leading edge, the local skin friction coefficient is C f , x = 0.0066. What is the value of the local Nusselt number at the same location if the Prandtl number is Pr = 7?
- Consider a 0.38m long vertical plate that is at 70°C. The plate is suspended in quiescentair that is at 25°C. Estimate the velocity boundary layer thickness and maximum upwardvelocity at the trailing edge of the plate. How does the boundary layer thickness comparewith the thickness that would exist if the air were flowing over the plate at a free streamvelocity of 6.8 m/s?A 20 °C water flows to 50cmx60cm flat plate with velocity of 6m/s . The flat plate surface temperature is maintained at 40 °C . The air flows parallel to the 50cm side of the plate. If the kinematic viscosity of water is 78x10-8 m2/s, at what length the flow become turbulent? If the average laminar heat transfer coefficient of water is 7740W/m2 °C , what is the overall heat transfer at the laminar section?A 20degC water flows to 50cmx60cm flat plate with velocity of 6m/s . The flat plate surface temperature is maintained at 40deg C. The air flows parallel to the 50cm side of the plate. If the kinematic viscosity of water is 78x10-8 m2/s, at what length the flow become turbulent? If the average laminar heat transfer coefficient of water is 7740W/m2 degC, what is the overall heat transfer at the laminar section?
- Consider an infinitely thin flat plate of chord c at an angle of attack α in asupersonic flow. The pressures on the upper and lower surfaces aredifferent but constant over each surface; that is, pu(s) = c1 andpl (s) = c2, where c1 and c2 are constants and c2 > c1. Ignoring the shearstress, calculate the location of the center of pressure.A hot-film probe is mounted on a cone-and-rod system in a sea levelairstream of 45 m/s, as in Fig. Estimate the maximumcone vertex angle allowable if the flow-induced bendingmoment at the root of the rod is not to exceed 30 N .cm.An 16-kg slab slides down a 25° inclined plane on a 4-mmthick film of SAE 30 oil at 15.6 °C; the contact area is0.3m2. Find the terminal velocity of the slab. Explain ur answer