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Understanding how the coefficient of lift ( CLcap C sub cap L ) and coefficient of drag ( CDcap C sub cap D ) dictate fuel efficiency and glider ratios. The Drag Polar: The fundamental equation relates parasite drag to induced drag. 2. Aircraft Performance Metrics

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Before looking at the numbers, draw a free-body diagram of the aircraft in the specific flight condition (climb, cruise, or turn). A key feature of John D

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