Helicopter rotor dynamics by finite element time approximation
نویسندگان
چکیده
منابع مشابه
Computational-Fluid-Dynamics- and Computational-Structural-Dynamics-Based Time-Accurate Aeroelasticity of Helicopter Rotor Blades
A modular capability to compute dynamic aeroelastic characteristics of rotor blades using the Euler/Navier– Stokes flow equations and finite element structural equations is presented. The approach is based on a time-accurate analysis procedure that is suitable for nonlinear fluid–structure interaction problems. Fluids and structural solvers are time-accurately coupled in the C++ environment. Un...
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ژورنال
عنوان ژورنال: Computers & Mathematics with Applications
سال: 1986
ISSN: 0898-1221
DOI: 10.1016/0898-1221(86)90092-1