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Question 1: What method is typically used to determine the aerodynamic stability of an aircraft during high-speed flight?

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Question 2: What is the primary benefit of using finite element analysis (FEA) in the design of aircraft structures?

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Question 3: What is the role of "winglets" in the structural design of an aircraft's wings?

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Question 4: In electrical systems design, why is redundancy critical in the power distribution network of a commercial aircraft?

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Question 5: What is the relationship between drag coefficient and Reynolds number in the design of aircraft components?

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Question 6: How does the pressure distribution over an aircraft wing affect its lift generation?

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