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- W2373472538 abstract "It is important to development one precise measurement technique and analysis methods of in-flight loads for aeroplane,by which could control test safely,advance flight-test efficiently,support design better and its optimize.So an analysis methods of wing loads in-flight is presented,by this method the distribution of aeroplane structure loads in whole flight envelop be can analysis.Subsequently the method is validated,and the result is discussed." @default.
- W2373472538 created "2016-06-24" @default.
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- W2373472538 date "2011-01-01" @default.
- W2373472538 modified "2023-09-24" @default.
- W2373472538 title "An Analysis Method of Wing Loads In-flight for Symmetry Maneuver" @default.
- W2373472538 hasPublicationYear "2011" @default.
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