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The largest load that is expected to be experienced by aircraft is called __________

(a) limit load

(b) normal stress

(c) normal strain

(d) shear stress

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I need to ask this question from Loads Categories topic in portion Structures and Loads of Aircraft Design

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Correct answer is (a) limit load

The explanation is: Limit load is the largest load that is expected to be experienced by aircraft. Shear force will produce shear stress. Stress is force per unit area and strain is defined as change in dimensions divided by original dimension.

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