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- W2394181447 abstract "Gust load of airplanes,especially of canard airplanes, is analysed and calculated when the airplane pitch is taken into account.The differential equations of the airplane motion in a gust are deduced based on the assumptions that the airplane can pitch with the life increment of the horizontal tail considered. The life increment caused by the airplane pitching is considered. These are different from the assumptions of NACA R1206.It is found that for static stability airplanes especially for canard airplanes which usually have the first stalling characteristics of the canard surface,the airplane pitching causes a little effect on the maximum gust load factor,although the airplane takes rather more time for penetrating a gust wave. The two-seat canard airplane AD200 is taken as an example. The result shows that the airplane pitching in a gust has a negligible effect on the gust-load for light canard airplanes." @default.
- W2394181447 created "2016-06-24" @default.
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- W2394181447 date "1994-01-01" @default.
- W2394181447 modified "2023-09-23" @default.
- W2394181447 title "Gust Load Calculation of Canard Airplanes with Pitching" @default.
- W2394181447 hasPublicationYear "1994" @default.
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