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Which one of the following statements about the lift-to-drag ratio in straight and level flight is correct?

Which one of the following statements about the lift-to-drag ratio in straight and level flight is correct?

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Related questions

1) At higher altitudes, the stall speed (IAS):


2) Shock stall is:


3) The critical angle of attack:


4) Which of the following will reduce induced drag?


5) Which one of the following statements about the lift-to-drag ratio in straight and level flight is correct?