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An aircraft material should be resistant to ______________

(a) join

(b) work

(c) shock loads

(d) strength

This question was posed to me by my school teacher while I was bunking the class.

Asked question is from Materials Selection in portion Materials Selection of Aerospace Materials & Processes

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Correct answer is (c) shock loads

For explanation I would say: An aircraft should be resistant to shock loads. Joining property and working property are important for the design and fabrication of components. Strength is an advantageous property for a material.

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