A wing is to be loft with span as 2m and reference area of wing is 4m^2. If we want to design the wing with taper ratio of 0.6 then what will be the value of tip chord?(a) 2.5m(b) 2.50m(c) 2.65m(d) 25.6mThis question was posed to me during a job interview.I would like to ask this question from Configuration Layout topic in portion Configuration Layout and Loft of Aircraft Design

A wing is to be loft with span as 2m and reference area of wing is 4m^

1.	A wing is to be loft with span as 2m and reference area of wing is 4m^2. If we want to design the wing with taper ratio of 0.6 then what will be the value of tip chord?(a) 2.5m(b) 2.50m(c) 2.65m(d) 25.6mThis question was posed to me during a job interview.I would like to ask this question from Configuration Layout topic in portion Configuration Layout and Loft of Aircraft Design
Answer» Correct CHOICE is (a) 2.5m Easiest explanation: GIVEN, SPAN b=2m, area S = 4m^2, TAPER ratio t = 0.6 Now, root CHORD Cr is given by, Cr = 2s / b (1+t) = 24 / 2(0.6+1) = 8/2*1.6 = 2.5m.

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