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Question 1: In designing the aircraft hydraulic system, what is the primary concern when selecting components for high-pressure applications?

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Question 2: How does prototype development address the need for rapid adaptability in military aircraft design?

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Question 3: In the context of prototype aircraft testing, what is the purpose of conducting a tailstrike test?

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Question 4: How do you handle the integration of newly designed control surfaces into the aircraft during flight testing?

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Question 5: When designing aircraft cabin systems, what is a primary factor in ensuring passenger safety during turbulence?

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Question 6: What method is most commonly used to evaluate the impact of stress concentrators, such as holes or notches, in an aircraft structure?

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