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Airplane Design Part VI : Preliminary Calculation of Aerodynamic Thrust and Power Characteristics,New
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Airplane Design Part VI: Preliminary Calculation of Aerodynamic, Thrust and Power Characteristics is the sixth book in a series of eight volumes on airplane design.The airplane design series has been internationally acclaimed as a practical reference that covers the methodology and decision making involved in the process of designing airplanes.Educators and industry practitioners across the globe rely on this compilation as both a textbook and a key reference.Airplane Design Part VI: Preliminary Calculation of Aerodynamic, Thrust and Power Characteristics, familiarizes the reader with the following fundamentals: Methods for estimating airplane drag with and without flaps Methods for estimating airplane lift with and without flaps Methods for estimating airplane pitching moment with and without flaps Methods for estimating installed thrust and power data Methods for estimating stability derivatives Methods for estimating control derivatives Methods for estimating hingemoment derivatives
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