Find span of wing is required in airplane

Reference no: EM13721311

Please determine the right solution of the given Problem

Problem- An airplane wing is to be designed to lift 2000 lb when the airplane is cruising at 200 ft/s with an angle of attack of 3^o.

Part 1- If the chord length is to be 4 ft, what span of wing is required (assuming standard atmospheric conditions).

I want experts assist to find span of wing is required in airplane.

Reference no: EM13721311

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