Articulated Rotor Blade Flapping Motion at Low Advance Ratio

By Harris Franklin D.  

Journal of the American Helicopter Society, Vol. 17, Iss. 1, 1972-01 ,pp. : 41-48

AHS International

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Analysis of the Stability of a Flexible Rotor Blade at High Advance Ratio

By Perisho Clarence H.  

Journal of the American Helicopter Society, Vol. 4, Iss. 2, 1959-04 ,pp. : 4-18

AHS International

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The Effect of Positive Pitch-flap Coupling (Negative δ₃) on Rotor Blade Motion Stability and Flapping

By Gaffey Troy M.  

Journal of the American Helicopter Society, Vol. 14, Iss. 2, 1969-04 ,pp. : 49-67

AHS International

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Rotor Blade Motion in a Vertical Sharp-edged Gust: A Study of the Dynamics of Helicopter Blade Flapping with a Method of Deriving Maximum Gust Deflexion

By Payne P.R.  

Aircraft Engineering, Vol. 26, Iss. 1, 1993-12 ,pp. : 10-14

Emerald Group Publishing Ltd

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Rotor Blade Motion in a Vertical Sharp-Edged Gust: A Stud/ of the Dynamics of Helicopter Blade Flapping with a Method of Deriving Maximum Gust Deflexion

By Payne P.R.  

Aircraft Engineering, Vol. 26, Iss. 3, 1993-12 ,pp. : 80-84

Emerald Group Publishing Ltd

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