Project 2 Unit Number: 301023 Unit Name: Advanced Thermal and Fluid Engineering Instruction ? Students will use ANSYS Fluent software to solve heat transfer problems in this project. ? The report must be in the format of Microsoft Word file and submitted through vUWS. Reports in hard copy will not be accepted. Note: Plagiarism Plagiarism is absolutely unacceptable. If plagiarism is suspected to be involved in a report, it will be reported to the school for further investigation. Late submission - Submitting the report late due to your own internet connection problem will be treated as late submission without a valid reason. To avoid delay, you need to submit the report well before the due date.Fins are popularly used to keep the temperature of electric devices low. This project is aimed to find out the best configuration of the fins as shown in Figure 1. Figure 2 is the design of the fins. The key parameters are: The surface of the fins including the base releases heat of 100 W. It is assumed that the heat flux is evenly distributed along all the fins surfaces shown in Figure 2 (excluding the bottom surface). A fan is used to blow air into the inlet and it is assumed that the air velocity is constant in the inlet duct. Figure 1 The setup of the whole system of a fin in a boxFigure 2 The design of the fins (unit: mm) Assignment 1. If the air flow velocity at the inlet is 1 m/s and the air temperature is 20°C. The fins are parallel to the x-direction in Figure 1, find out which of the follow configuration leads to the lowest temperature on the fin: a. The centres of the inlet and outlet ducts are 70 mm above the bottom. b. The centres of the inlet and outlet ducts are 850 mm above the bottom. c. The centres of the inlet and outlet ducts are 100 mm above the bottom. 2. Using the best height of the air duct found in question 1, find which of the following configuration has the lowest temperature on the fin: a. The...
Already registered? Login
Not Account? Sign up
Enter your email address to reset your password
Back to Login? Click here