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This project requires knowledge of dynamics and aircraft motions, as well as conditions for static flight balance and flight stability, implying knowledge and methods of how the principal forces acts on the whole aircraft. The Assignment is made up two parts : Part A : which contains 5 questions about Information of Balance and stability in an aircraft using equations and graphs. Part B: which contains 5 questions about equations of motion and strip theory about an aircraft. I would appreciate it if the answers could be given from a computer via a word document, but i wouldn’t mind hand written answers

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