The Rotating Beam Problem In Helicopter Dynamics (foundations Of Engineering Mechanics)
by Ranjan Ganguli /
2017 / English / PDF
4.6 MB Download
The book addresses computational methods for solving the problem
of vibration, response, loads and stability of a helicopter rotor
blade modeled as a rotating beam with flap or out-of-plane
bending. The focus is on explaining the implementation of the
finite element method in the space and time domain for the free
vibration, aeroelastic response and stability problems. The use
of Floquet analysis for the aeroelastic stability analysis of
rotor blades is also shown. The contents of the book will be
useful to researchers in aerodynamics and applied mechanics, and
will also serve well professionals working in the aerospace
industry.
The book addresses computational methods for solving the problem
of vibration, response, loads and stability of a helicopter rotor
blade modeled as a rotating beam with flap or out-of-plane
bending. The focus is on explaining the implementation of the
finite element method in the space and time domain for the free
vibration, aeroelastic response and stability problems. The use
of Floquet analysis for the aeroelastic stability analysis of
rotor blades is also shown. The contents of the book will be
useful to researchers in aerodynamics and applied mechanics, and
will also serve well professionals working in the aerospace
industry.
