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Question 1: How do you determine the factor of safety for a thin-walled cylindrical structure under internal pressure?

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Question 2: When designing a lightweight, high-performance aircraft, what is the primary challenge in achieving structural integrity?

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Question 3: How do you determine the wing loading for an aircraft during the design process?

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Question 4: What method is most commonly used to analyze stress concentration around a hole in an aircraft skin under tensile loading?

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Question 5: What is the importance of aerodynamic shaping in the structural design of an aircraft?

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Question 6: Which type of electrical connector is typically used for high-reliability aerospace applications?

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