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- W2363424236 abstract "Based on analyzing the principle of reduced thrust,process and limitation of reduced thrust were studied,and temperature characteristics of turbine engine and influence of temperature to thrust was researched,and the plot of height,temperature versus thrust of a commercial aircraft was drawn.In order to research Assumed Temperature and its influence on fuel consumption and take-off performance,the control law based on optimal servo for turbine engine was designed.Furthermore,the system model was built in virtue of MATLAB / SIMULINK toolbox,the vertical control law of Assumed Temperature Method was simulated,and the simulation curves were offered.Results show that the Assumed Temperature earns big benefits from reducing fuel consumption and reduces operating costs of airline effectively." @default.
- W2363424236 created "2016-06-24" @default.
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- W2363424236 date "2013-01-01" @default.
- W2363424236 modified "2023-09-23" @default.
- W2363424236 title "Research on Reduced Thrust Take-off of Large Passenger Aircraft Based on Assumed Temperature" @default.
- W2363424236 hasPublicationYear "2013" @default.
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