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For a given aircraft, flying in straight and level flight, maximisation of the l...

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For a given aircraft, flying in straight and level flight, maximisation of the lift-to-drag ratio (L/D) means

Minimum drag, since lift is fixed by weight

100%

Maximum lift, since drag is fixed by thrust

0%

Maximum thrust, since lift is fixed by weight

0%

Minimum weight, since thrust is fixed by drag

0%

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