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Mechanical Assigment 1 Add in library

Referencing Styles : Harvard
Question 1 A group of engineering students are venturing to build a human powered aircraft as shown in Fig .1. The aircraft is to be designed with a wing span of 30 meters to achieve sufficient lift. The main load bearing element on the wing is an aluminium spar that extends along the length of the wing. The cockpit and supporting structures (without the wing) is expected to weigh AB kg excluding a pilot of 70 kg, the propeller mass is BC kg. Accordingly, to aid with the design of the wing appl ...

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Tags: United Kingdom Wolverhampton Engineering Engineering Mechanical Engineering University of Wolverhampton Engineering Mechanics I 4ET003 

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