Consider a thin,
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Fundamentals of Heat and Mass Transfer
- Neatly handwritten solution requiredarrow_forward7.17 Air at a pressure of 1 atm and a temperature of 50°C is in parallel flow over the top surface of a flat plate that is heated to a uniform temperature of 100°C. The plate has a length of 0.20 m (in the flow direction) and a width of 0.10 m. The Reynolds number based on the plate length is 40,000. What is the rate of heat transfer from the plate to the air? If the free stream velocity of the air is doubled and the pressure is increased to 10 atm, what is the rate of heat transfer?arrow_forwardExperimental measurements of the convection heat transfer coefficient for a square bar in cross flow yielded the following values: Assume that the functional form of the Nusselt number is Nu = C*Rem*Prn, where C, m, and n are constants. Also, assume that air temperature does not change in the following problem.A. What will be the convection heat transfer coefficient for a similar bar with L = 1 m when V = 15 m/s?B. What will be the convection heat transfer coefficient for a similar bar with L = 1 m when V = 30 m/s?arrow_forward
- In elementary mechanical fluidarrow_forwardAir at 200C and at a pressure of 1 bar is flowing over a flat plate at a velocity of 3 m/s. If the plate is 280 mm wide and at 560C, calculate the following quantities at x = 280 mm given that properties of air at the bulk mean temperature 20 + 56/2= 380C are: (i) Boundary layer thickness,(ii) Local friction coefficient,(iii) Average friction coefficient,(iv) Shearing stress due to friction(v) Thickness of the boundary layer,(vi) Local convective heat transfer coefficient,(vii) Average convective heat transfer coefficient,(viii) Rate of heat transfer by convection(ix) Total drag force on the plate, and(x) Total mass flow rate through the boundaryarrow_forwardAir flow across a cooling fin: A 35 mm (in the streamwise direction) aluminum cooling fin has a temperature of 54 C and needs to be cooled to 44 C using cross flow. The fin is surrounded by air and must be cooled with laminar flow to minimize the boundary layer thickness and reduce aerodynamic drag. 1. What is the fastest fluid velocity that can be used to keep the flow laminar? 2. If the flow velocity drops 10% and the frictional force is decreased by 20%, by what percentage would you expect the heat transfer to drop?arrow_forward
- Problem 1. A smooth plate with length L = 3.0 m and width b = 0.90 m moves through still air at STP at a velocity of U = 4.5 m/s that is aligned with L. Calculate the following for a boundary layer that stays laminar and for one that trips to turbulent at the leading edge: (a) boundary layer disturbance thickness, 8, at x = 0.5, 1.0, 1.5, 2.0, 2.5, and 3.0 m from the leading edge of the plate, (b) wall shear stress, Tw, at those æ- locations, and (c) friction drag, Fp.f, on one side of plate. (d) Calculate percent decrease in drag for laminar versus turbulent boundary layer.arrow_forward8- Air (p = 1.21 kg/m') flows over a thin flat plate 1 m long and 0.3 m wide. The flow is uniform at the leading edge of the plate. Assume the velocity profile in the boundary layer is linear, and the free stream velocity is 2.7 m/s. Using control volume (abcd) shown in figure, compute the mass flow rate across surface (ab). Determine the magnitude and direction of the x- component of the force required to hold plate stationary. [3.9×10 kg/s ; -3.5x10 N]arrow_forward6- A uniform free stream of air at 0.8 m/s flows over a flat plate (4 m long x 1 m wide). Assuming the boundary layer to be laminar on the plate and the velocity profile is: Find the ratio of the drag force on the front half portion to the drag U. 2 force on the rear half portion of the plate. (p = 1.2 kg/m; v = 1.51x10 m²/s) [2.42]arrow_forward
- Problem 9. Assume that we want to model a recirculating flow happens at the downstream of a step as shown in the following sketch. (a) Specify the position of reattachment point and the appropriate distance of the outflow boundary layer, as a function of step height, h. (b) Determine all of the required boundary conditions for turbulent parameters (k and D) in each boundary. (c) Which turbulence model do you suggest to solve this problem? h ?arrow_forwardQuestion 9 Consider the flow of water over a flat plate. In a different experiment consider the flow of air over a flat plate. In both cases the flow is steady, the boundary layers that are formed are laminar and the gravitational acceleration can be neglected. In both cases the velocity far from the plates is the same (v.) and the temperature is also the same (80 °F). For the same distance x from the leading edge, in which boundary layer will the friction coefficient be higher? (a) The friction coefficient is the same for both cases. (b) In water. (c) In air. (d) It depends on the velocity profile that is assumed inside the boundary layer.arrow_forwardHelp me step by steparrow_forward
- Principles of Heat Transfer (Activate Learning wi...Mechanical EngineeringISBN:9781305387102Author:Kreith, Frank; Manglik, Raj M.Publisher:Cengage Learning