Improvement of aeroelastic stability of hingeless helicopter rotor blade by passive piezoelectric damping
نویسندگان
چکیده
منابع مشابه
Helicopter Blade Stability Analysis Using Aeroelastic Frequency Response Functions
In the present paper, the aeroelastic stability of helicopter rotor blade is determined using Aeroelastic Frequency Response Function. The conventional methods of aeroelastic stability usually use an iterative procedure while the present method does not require such approach. Aeroelastic Frequency Response Functions are obtained by inverting dynamic stiffness matrix of the aeroelastic system. S...
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ژورنال
عنوان ژورنال: International Journal of Aeronautical and Space Sciences
سال: 2006
ISSN: 2093-274X
DOI: 10.5139/ijass.2006.7.1.054