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- W2355563592 abstract "The methods were studied for predicting range and endurance of a propeller plane at constant altitude. When the thrust coefficients of fuel consumption are constant, the calculation formulas of optimal cruise states (including posture and airspeed) were presented when long-range and long-endurance were demanded, and the calculation formulas of range and endurance were given when flight strategy is holding airspeed or posture uniformly. We conclude that variable posture and variable airspeed of a plane were needed for long-range flight, and changeless posture and variable airspeed were needed for long-endurance flight." @default.
- W2355563592 created "2016-06-24" @default.
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- W2355563592 date "2003-01-01" @default.
- W2355563592 modified "2023-09-27" @default.
- W2355563592 title "Calculation of Range and Endurance of a Propeller Aircraft at Constant Altitude" @default.
- W2355563592 hasPublicationYear "2003" @default.
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