DYNAMIC LOADS OF CONTROL SYSTEM ELEMENTS

摘要

The aim of this article is to give an advisable engineering method applicable to the calculation forces and moments arriving from the rotor side and arisen from the aerodynamic and dynamic effects over the rotor blades. Aerodynamic forces and moments can be estimated by the using of the integrated blade and impulse theory while the unsteady effects and compressibility of the flow can be considered in the blade element theory.