Abstract
In this chapter we will examine a number of aeroelastic phenomena associated with helicopters and other rotor or propeller driven aircraft. Certain areas have been selected for treatment to illustrate some significant stability problems which are associated with the design of helicopters. The approach to be followed employs simplified modelling of various problems such that physical insight into the nature of the phenomena can be obtained. In general a complete and precise formulation of many of the problem areas discussed is highly complex and the reader is referred to the literature for these more detailed formulations.
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Crawley, E.F., Curtiss, H.C., Peters, D.A., Scanlan, R.H., Sisto, F. (1995). Aeroelastic response of rotorcraft. In: Dowell, E.H. (eds) A Modern Course in Aeroelasticity. Solid Mechanics and its Applications, vol 32. Springer, Dordrecht. https://doi.org/10.1007/978-94-011-0499-9_7
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DOI: https://doi.org/10.1007/978-94-011-0499-9_7
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