q5 Atmospheric air at25hows over a fiat plate at a velocity of o ms The ter...
Supplemental Problem 7.001 A flat plate of width 1 m is maintained at a uniform surface temperature of Ts = 160°C by using independently of thickness a 12 mm and length b 50 mm. plate at a velocity of 30 m/s. The thermophysical properties of the module are k Reynolds number is 5x105 rectangular modules Each module is insulated from its neighbors, as well as on its back side. Atmospheric air at 25%C flows over the 5.2 w/m-K, cp320 J/kg...
PRINTER VERSION BACK NEXT RCES Supplemental Problem 7.001 A flat plate of width 1 m is maintained at a uniform surface temperature of T,-160°C by using independently controlled, heat-generating rectangular modules of thickness a 10 mm and length b 50 mm. Each module is insulated from its neighbors, as well as on its back side. Atmospheric air at 25°C flows over the plate at a velocity of 30 m/s. The thermophysical properties of the module are k5.2 W/m K, cp...
A thin, flat plate of 0.6 m square is immersed in a parallel stream of air at atmospheric pressure and 15 ºC flowing at a velocity of 6 m/s. Neglect edge effects. a) Determine the drag force exerted on the plate. b) Determine the boundary layer thickness and the local drag coefficient at a distance 0.3 m from the leading edge.
Air at atmospheric pressure and temperature of 56 5 C flows with velocity of 0915 m/sec along a flat plate which is kept at a uniform temperature of 121.C Determine the local heat transfe coefficient hx) at a distance of 0.61 meter from the leading edge of the plate and the t transfer coefficient h. over the length of 0to061m peer feet of plate width Air at average temperature has Pr 062, 00313 W/m. C and u 0.22310 m/se
RCES Problem 7.002 Engine oil at 100°C and a velocity of 0.20 m/s flows over both surfaces of a 1-m-long flat plate maintained at 20°C 001 Determine: (a) The velocity and thermal boundary layer thicknesses at the trailing edge. (b) The local heat flux and surface shear stress at the trailing edge. (c) The total drag force and heat transfer per unit width of the plate. 02 Determine the velocity boundary layer thickness 6 at the trailing edge, in m....
Consider liquid water flowing over a flat plate of length L = 1 m. The water has the following properties: ρ-1000 kg/m3, Cp-4000 J/kgK. 10 3 kg/ ms, k 0.6 W/m . C μ Midway through the plate at x = 0.5 m, you measure a heat flux to the surface of: 05 m 3181 W/m2 You also measure an average heat flux to the surface over the length of the plate of: "4500 W/m2 Knowing the latter, and knowing...
Air at atmospheric pressure and temperature of 565 C flows with velocity of 0915 m/sec along a flat plate which is kept at a uniform temperature of 121.1 C. Determine the local heat transfer coefficient hk) at a distance of 0,61 meter from the leading edge of the plate and the total heat transfer coefficient hm over the length of x 0 to x= 0.61m peer feet of plate width. Air at average temperature has Pr 0.62, k-0.0313 W/m. C...
Heat Transfer Please be neat and organized for a thumbs up! Problem 3 Atmospheric air at T 300 K and a free stream velocity of u 10 m/s flows over a flat plate L = 2 m long that is maintained at a uniform temperature T-320 K. (a) Calculate the average heat transfer coefficient over the region where the boundary layer is laminar. What is the boundary layer thickness at this location? plate as well as the velocity boundary layer...
Air flows with a velocity of 20 m/s over a flat plate of length 2 m. The air properties are k = 0.030 W/mK, V = 20.92 x 10-6 m/s, Pr=0.700. a. What type(s) of flow (laminar/turbulent) exist on this plate? b. If the following relations are given for the laminar and turbulent local convection coefficients over the plate, haminar (x) = 20 houwbudemo (x) = .52 where x is the distance from the plate leading edge. Find the average...
8) Air flows over a flat plate at a velocity of 20 m/s and a temperature of 20C. The surface temperature of the plate is 134C, and the length of the plate in the direction of flow is 1.5 m. Properties of air may be taken as A-0.030 W/m-C, Pr-0.700, and a/p 2.092E-5 m/s (5% ) What is the location from the leading edge, X, where the flow becomes turbulent Re (20)15 a l Ve30s T20 T LaLS 523 m...