6- Air at a pressure of 200 kPa and free-stream temperature of 27 C flows over a square flat plate at a velocity of 30 m/s. The Reynolds number is 10° at the edge of the plate. Calculate the heat transfer for an isothermal plate maintained at 57 C. v = 8.6x106 k = 0.0274; Pr = 0.7 Nu = 1299 Answers: q = 676W
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- Air at 20 ◦ C flows inside a pipe 18-mm-ID having a uniform heat flux of 150 W/m 2 on the surface, the average flow velocity at entry being 1.0 m/s. The air pressure is 2 bar. Determine the value of convection coefficient. If the pipe is 2.5 m long, determine the air exit temperature and the wall temperature at the exit. Assume fully developed hydrodynamic boundary layer.A steam reservoir is covered by a rectangular plate (its length is 1 m and width 2 m). The steam temperature is 95o C, and it is in contact with the plate. Over the outside surface of the plate, water is flowing at a speed of 3 m/sec at a temperature of 25o C. What is the mean Nusselt number over the plate? What is the mean heat transfer convective coefficient over the plate? What is the heat transfer rate to the water?Atmospheric air is in parallel flow (u∞ = 10 m/s, T = 15°C) over a flat heater surface that is to be maintained at a temperature of 90°C. The heater surface area is 0.25 m², and the airflow is known to induce a drag force of 0.17 N on the heater. What is the electrical power, in kW, needed to maintain the prescribed surface temperature? Use the modified Reynolds or Chilton-Colburn analogy. Evaluate properties for the air at 325 K. q= i kW
- Outside air ( v =15.89 x 10-6 m²/s, p= 1.16 kg/m³, Pr=0.707, k=0.0263 W/mK) with temperature of T-12 °C flows over a flat glass window (kglass=1.05W/mK) with L=0.5m lengtl the air velocity is measured as U=1.25 m/s and the glass thickness is t= 50 mm, calculate: 1. Reynolds number at the glass edge (i.e. point A)-Is the flow laminar or turbulent? 2. Average shear stress on outer surface of the glass 3. Velocity boundary layer thickness at the glass edge (point A) 4. Average convective heat transfer coefficient on outer surface of the glass AConsider two cases involving parallel flow of dry air at V = 4.5 m/s, T, = 45°C, and atmospheric pressure over an isothermal plate at T = 20°C. In the first case, Re= 5x 105, while in the second case the flow is tripped to a turbulent state atx = 0 m. At whatx -location, in m, are the thermal boundary layer thicknesses of the two cases equal? What are the local heat fluxes, in W/m?, at this location for the two cases? x = i m Jam i W/m? i W/m? I turbAir flowing over a 1-m-long flat plate at a velocity of 7 m/s has a friction coefficient given as Cf= 0.664(Vx/v) is the location along the plate. 1-0.5 where x Given:/The properties of air at 20°C are u = 1.825 × 10 kg/m-s, V =1.516 × 105 m-/s, and p= 1.204 kg/m -5 Determine the wall shear stress at x 0.6 m of the plate. Evaluate the air properties at 20°C and 1 atm. (Round the final answer to five decimál places. You must provide an answer before moving on to the next part.) The wall shear stress is | Nim2.
- A pressurized gas at a pressure of 7 kPa and temperature of 30°C flows across a 0.3 x 0.3 m² flat plate at 7.45 m/s. The plate is maintained at 70°C. Estimate the heat lost from the plate. Given: µ=2.025x10$ kg/m,s, k=0.02798 W/m.°C Pr = 0.709 , p= 0.0754 kg/mAir with free stream temperature of 10 C is flowing over a flat plate (1.5m long and Im wide). The air is flowing along 1.5m side of the plate. The plate is maintained at 90 C. Find the velocity of air required to have a rate of heat dissipation as 3.75 kW. Use the correlations: Nu =0.664Res Pro3 for laminar flow Nu, = (0.037R *-871)Pr for turbulent flow Take the properties p = 1.0877 kg/m u=2.029x10 m/s, k=0.028 W/mK, C,-1.007KJ/kg.K and Pr=0.703 %3DThe exact expression for the local Nusselt number for laminar flow along a flat plate is given by: Nux=h(x)x/k=0.332Pr1/3Rex1/2. Atmospheric air at Tinf=400K with a velocity uinf=1.5m/s flows over a flat plate L=2m long maintained at a uniform temperature Tw=300K. Calculate the heat transfer rate from the airstream to the plate from x=0 to x=L=2m for w=0.5m. A. 234 W B. 334 W C. 434 W D. 134 W
- 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?A 4m x 4m flat piale maintained at a constant temperature of NOC is subjected to parallel flow of nit at I am. 20 ', and 10 m's. The total drag force acting on the upper surface of the plate is measured to be 2.4N Determine the average convection hear transfer coefficient, and the rate of heat transfer between the upper surface of the plate and the air. The properties of air at 20 ° C and 1 atm from tables, areA heat treat steel plate measures 3 m *1 m and is initially at 30 degree Celsius. It is cooled by blowing air parallel to 1 m edge at 9 km/hr. If the air is at 10 degree Celsius. Estimate the convective heat transfer from both sides of the plate.