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Estimating % Power using Flight Test Data, Thrust HP, and Equivalent Flat Plate Drag

Estimating % Power using Flight Test Data, Thrust HP, and Equivalent Flat Plate Drag. Objective. The Objective is to generate a Chart that relates: RPM % Power Output True Airspeed Fuel Flow Range Cruise Altitude. Methodology.

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Estimating % Power using Flight Test Data, Thrust HP, and Equivalent Flat Plate Drag