25th Congress of International Council of the Aeronautical Sciences, 3 - 8 September 2006, Hamburg, Germany
Paper ICAS2006-10.6S

DYNAMIC LOADS OF CONTROL SYSTEM ELEMENTS

T. Gausz, Z. Gausz
Budapest Univ. of Technology and Economics, Hungary

Keywords: control loadings, rotor blade, dynamics

In this article is present a recommendable investigation method of dynamic loads of control system elements. The estimation of loads is based on the helicopter rotor dynamics. Aerodynamic forces and moments are calculated by the blade element and impulse theory. The elastic deformations are estimated too.

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