Question: A wing is to be loft with span as 2m and reference area of wing is 4m2. If we want to design the wing with taper ratio of 0.6 then what will be the value of tip chord?

Options

A : 2.5m

B : 2.50m

C : 2.65m

D : 25.6m

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Configuration Layout - Vulnerability Considerations more questions

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Consider below wing. Calculate the value of span of wing....

If an aircraft has three components which can be considered....

In order to improve vulnerability consideration, we can use ___

Term marked by '?' in diagram is __^

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