Investigations on the Effect of Blade Torsion on the Dynamics of the Flapping Motion

ISSN： 2161-6027

Source： Journal of the American Helicopter Society, Vol.15, Iss.2, 1970-04, pp. : 2-9

Disclaimer: Any content in publications that violate the sovereignty, the constitution or regulations of the PRC is not accepted or approved by CNPIEC.

Previous Menu Next

Abstract

Related content

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

Access to resources Recommend Favorite

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

Access to resources Recommend Favorite

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. 2, 1993-12 ,pp. : 41-45

Emerald Group Publishing Ltd

Access to resources Recommend Favorite

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

Access to resources Recommend Favorite

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

Access to resources Recommend Favorite