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- W28958902 abstract "This chapter discusses two applications of the longitudinal stability equations. These are the response to elevator angle and the response to a gust or a distribution of random gusts. The chapter particularly is concerned with finding the normal acceleration of both the cg and various points of the aircraft. The ultimate purpose of the chapter is to provide information to design an aircraft which is safe to fly and fully capable of achieving its missions. The chapter is divided into sections. The first one deals with the response to elevator movement. It studies the elevator responses to determine how quickly maneuvers can be performed and what loads and hence stress levels may be imposed on the aircraft. Two methods are worthy of consideration; the first uses the Laplace transform and the second uses numerical integration of the equations in state–space form. The corresponding frequency responses are also of great interest. The second section discusses the response to gusts. It studies the response to gusts to determine the effect on passenger comfort or the suitability of the aircraft as a weapons platform. It also aims to study the effects on the stress levels and fatigue life of the airframe." @default.
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- W28958902 date "1996-01-01" @default.
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- W28958902 title "Longitudinal response" @default.
- W28958902 doi "https://doi.org/10.1016/b978-034063170-6/50012-8" @default.
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