This chapter outlines briefly some of the processes employed in the commercial aerospace industry for aeroelastics and loads analysis with reference made to the certification specifications. The aeroelastic and loads behaviour of the aircraft have an impact upon the concept and detailed structural design, aerodynamic characteristics, weight, jig shape, FCS design, handling qualities, control surface design, propulsion system, performance, landing gear design, structural tests, etc. It can be convenient to think of the design and development cycle as comprising a number of phases: concept phase, pre‐design phase, detailed design phase, and validation and certification phase. The certification of aircraft is a complex process and depends upon where in the world the aircraft is manufactured, and where it is to be purchased and operated.
Aircraft Design and Certification
2014-12-02
9 pages
Article/Chapter (Book)
Electronic Resource
English
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