Suppose an airliner is planning to fly an Airbus A319 very low over a water surface, thereby increasing its lift coeffic

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Suppose an airliner is planning to fly an Airbus A319 very low over a water surface, thereby increasing its lift coeffic

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Suppose an airliner is planning to fly an Airbus A319 very lowover a water surface,thereby increasing its lift coefficient by 40%. However, theairliner does not need 40%extra lift, instead it decides to reduce the wing area such thatthe aircraft generates thesame lift as a normal A319. What would the wing area (in squaremetres) of thismodified A319 have to be?
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