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  • Q1:EG-194 Introduction to Aerospace Engineering Assignment 1, 2023 This assignment should take the average student around 10 hours to complete to a good standard. It is expected that six to eight hours will be required to find, read and understand relevant material from a variety of sources. A well-written report that adheres to the format described below will probably take between two to four hours to write. The assignment title is: Discuss the advantages, disadvantages and prospects for aircraft using fuel-cells Notes, Format and Submission Fuel cells, using hydrogen or ammonia as a fuel for example, work like batteries, but they do not run down or need recharging, which is an option for future aircraft to reduce the emissions such as CO2. For example, the company ZeroAvia conducted a 10-minute test flight using an engine that converts hydrogen fuel into electricity to power one of the plane's two propellers. You are required to write a two-page paper on the topic of fuel-cell powered aircraft that includes a technical overview of one or more designs and details of how the design(s) address concerns such as life-circle assessment, safety, the environment or sustainability. There is no requirement to cover all the concerns listed. The paper should start with an introduction to the topic and briefly describe the concept of fuel-cell-powered aircraft. Additionally at this stage whichever life-circle assessment, safety, environmental and sustainability will play a part later in the paper should be explained in general. The main part of the paper should use one or more examples from current developments or research that relate to the essay topic and identify progress in the area. With any approach, there are normally advantages and disadvantages. Authors will usually tell you the advantages but you should also consider what the disadvantages of the approach are (why is the approach not being used at this time?). Also, consider how is the design addressing the area(s) of concern that you have focussed on? The paper should conclude by drawing together the issues described and suggesting the likely prospects for achieving the goals. A successful response to this assignment would be a well-organised and argued case that displays an understanding of the underlying issues related to aerospace engineering. You will have to be precise and selective with what you include as the format instructions below limit the space you have available. The assignment must be written in a word processing package and submitted electronically. The MAXIMUM LENGTH is 2 pages, using 12-point Times New Roman font and A4 paper size, all MARGINS must be at least 4 cm and single line spacing must be used. All pages should have a header with your name on the left and your student number on the right. The first page should have the assignment title (given above) as the title, in bold type. Any pictures or diagrams included used must be within the page and margin constraints given above. The length constraints mean that only a small number of sources are likely to be cited - any references should be included onSee Answer
  • Q2:5. Format of the report The report has a strict 4-page limit. Anything above four pages will be penalised according to the marking guidance. The report should contain a front sheet (which will not count towards the page limit), containing the following information only: Name Student ID Module Code Module Title • Coursework Name The report should be written as a formal lab report with appropriate headings. Do not include a table of contents or appendix. Do not repeat large sections from this handout in relation to the background or the procedures. As a rough guide, approximately three pages should cover the raw and processed data, with one page to cover a discussion of the flow physics. Note that the raw data should be presented to you in the units it was. Appropriate references are essential to show that you have engaged with and understood the data and the theory. The required format is single-spaced Times New Roman font, size 12 pt. The page margins should be set to normal, i.e. 2.54 cm at Top/Bottom/Left/Right.See Answer
  • Q3:Question 1 2 pts Question 1: In a wind tunnel test of flow over a wing section, air enters the test section at a speed of 54 m s1 and a pressure of 942 kPa. Assuming Bernoulli's principle applies to the flow, what is the pressure at the stagnation point on the wing surface if the air density is 1.16 kg m 3? The answer should have units of kPa.See Answer
  • Q4:9. Task B: B1: B2: B3: 15 marks) B4: As small AOA, how do you see C₂ varies with a ? As AOA increases, does the relationship you observes in B1 continues? Why? Is there any difference in the C₁ vs a relation you observed in B1, for airfoil with difference thickness, and different camber? At even higher AOA, what happen to the relationship between C₂ and a? In your own words, describes the flow phenomenon that has occurs. B5: Tabulate and discuss the Stall AOA and maximum C₂ of the 4 airfoil studied. B6: Compute and discuss the lift-curve slopes for the 4 airfoil studied. (15 marks)See Answer
  • Q5: =) Spanwise pressure coefficients are shown for 3 streamwise stations of a delta wing at two angle of attack conditions, a = 6.8° (top row) and a =16.3° (bottomrow). From these plots, explain the vortex behavior for each condition. See Answer

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