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- W2185655561 abstract "Each airplane is not only operated in a level steady flight, but also has to perform a number of maneuvers. Sometimes these maneuvers are very rapid and it is the reason that extreme loads generated in such maneuvers on the tailplanes have to be calculated. These loads are responsible for the state of strain, elastic deflection, fatigue and other phenomena. Among different maneuvers considered in this paper are motions following a sudden deflection of elevator and response to a vertical gust. This paper focuses mainly on the flight dynamics and flight control system of a trainer jet aircraft. Analysis is based on the linearized equation of motion of a rigid airplane of six degrees of freedom in an arbitrary motion with deflectable control surfaces. An important point in the analysis was estimating the stability derivatives, computed by means of panel methods, and compared with the results of classical engineering approach." @default.
- W2185655561 created "2016-06-24" @default.
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- W2185655561 date "2002-01-01" @default.
- W2185655561 modified "2023-09-27" @default.
- W2185655561 title "EXTREME LOADS OF A TRAINER JET FOLLOWING A SUDDEN DEFLECTION OF CONTROL SURFACE" @default.
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- W2185655561 hasPublicationYear "2002" @default.
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