This chapter discusses the different ways in which flight manoeuvres and gusts are handled in industry when seeking type certification. The wide range of different cases that have to be considered is examined. From these bookcase and rational design calculations, the internal loads can be determined which then are used to estimate the stresses. The chapter considers the cases of balanced equilibrium manoeuvres involving pitch, roll and yaw as bookcases. It examines the treatment of the aircraft when undergoing some form of dynamic manoeuvre. A considerable effort over many years has been put into deciding how to define the certification requirements for loads in gusts and turbulence, with the methodologies becoming ever more rational and complex. The aircraft model should include models for all relevant modes of any Flight Control System if any coupling with the structural response is possible.
Flight Manoeuvre and Gust/Turbulence Loads
2014-12-02
13 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
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