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Keywords: Finite‐element solution
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Journal Articles
Aircraft Engineering and Aerospace Technology: An International Journal (2012) 84 (6): 367–375.
Published: 12 October 2012
... Guide, 2008). In the finite‐element solution algorithm each beam element is allowed to be arbitrarily oriented, thus permitting the simulation of tip sweep and anhedral angles effects. Introducing a sectional theory corrected with a wake inflow model to evaluate the aerodynamic loads acting on the blade...
