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Question 1: What is the main advantage of using automated test systems in aerospace software development?

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Question 2: What are the key benefits and challenges of using "Finite Element Analysis" (FEA) in aerospace simulation software, particularly for structural integrity?

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Question 3: Which C++ feature can be used to minimize the impact of pointer arithmetic errors in aerospace systems?

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Question 4: How would you handle software requirements that change during the development cycle in an aerospace project?

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Question 5: In aerospace simulation, how does the "boundary layer" model help improve simulation accuracy?

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Question 6: How do "Code Reviews" improve the quality of C/C++ software in aerospace applications, and what techniques do you use to ensure that the reviews are effective?

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