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Question 1: How do you ensure that prototype testing is comprehensive and covers all potential flight conditions?

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Question 2: How does a change in the center of gravity (CG) affect the structural integrity of an aircraft during flight?

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Question 3: What role does computational fluid dynamics (CFD) play in optimizing the design of an aircraft prototype?

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Question 4: What is the purpose of performing a sideslip test during flight testing?

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Question 5: In a composite material, how does fiber orientation affect the material's stiffness?

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Question 6: In the context of airworthiness certification, what does the term "damage tolerance" refer to in aircraft structural design?

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