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A wing has chord of 1m. Find the appropriate range of the front spar position from l.e.(a) 0.2m-0.3m(b) 0.9m-1.5m(c) 3.2(d) 1.2I got this question in an interview.My question comes from Configuration Layout topic in division Configuration Layout Considerations of Aircraft Design

Answer»

Right answer is (a) 0.2m-0.3m

The explanation: Given chord c = 1m.

Typical range of front SPAR location = 20% to 30% of chord = 20% of 1 to 30% of 1 = 0.2*1 to 0.3*1 = 0.2m-0.3m.



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