NASA NTRS · 19910000263
Transonic Aeroelasticity Analysis For Helicopter Rotor Blade
Abstract
Numerical-simulation method for aeroelasticity analysis of helicopter rotor blade combines established techniques for analysis of aerodynamics and vibrations of blade. Application of method clearly shows elasticity of blade modifies flow and, consequently, aerodynamic loads on blade.
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Chang, I-Chung, Gea, Lie-Mine, Chow, Chuen-Yen. 1991-06-01. Transonic Aeroelasticity Analysis For Helicopter Rotor Blade. https://ntrs.nasa.gov/citations/19910000263
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