Find the wing reference area if wing loading is 85 lb/ft^2 and aircraft has gross weight of 10000 lb.(a) 117.64 ft^2(b) 112.65 ft^2(c) 152 ft^2(d) 125 ft^2The question was posed to me during an interview.Origin of the question is Geometry Sizing topic in division Initial Sizing of Aircraft Design

Find the wing reference area if wing loading is 85 lb/ft^2 and aircraf

1.	Find the wing reference area if wing loading is 85 lb/ft^2 and aircraft has gross weight of 10000 lb.(a) 117.64 ft^2(b) 112.65 ft^2(c) 152 ft^2(d) 125 ft^2The question was posed to me during an interview.Origin of the question is Geometry Sizing topic in division Initial Sizing of Aircraft Design
Answer» CORRECT choice is (a) 117.64 ft^2 To explain I WOULD say: Given, take-off GROSS weight is W0 = 10000 LB, wing loading W.L. = 85 lb/ft^2 W.L. = W0/area, area = W0/ W.L. = 10000/85 = 117.64 ft^2.

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Find the wing reference area if wing loading is 85 lb/ft^2 and aircraft has gross weight of 10000 lb.(a) 117.64 ft^2(b) 112.65 ft^2(c) 152 ft^2(d) 125 ft^2The question was posed to me during an interview.Origin of the question is Geometry Sizing topic in division Initial Sizing of Aircraft Design

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