Theoretical Damping in Roll and Rolling Effectiveness of Slender Cruciform Wings PDF Download
Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download Theoretical Damping in Roll and Rolling Effectiveness of Slender Cruciform Wings PDF full book. Access full book title Theoretical Damping in Roll and Rolling Effectiveness of Slender Cruciform Wings by Gaynor J. Adams. Download full books in PDF and EPUB format.
Author: Gaynor J. Adams
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 40
Get Book Here
Book Description
The coefficients of damping in roll and rolling effectiveness (with differential incidence of the horizontal surfaces) are determined for a slender, equal-span, cruciform wing. It is found that the coefficient of damping in ar roll is 62 percent greater than for a plane slender wing of equal aspect ratio, and that the rolling effectiveness is 53 percent less than for a plane slender wing of equal aspect ratio. The analysis can be used in the estimation of the characteristics of a slender, equal-span, cruciform wing having any specified distribution of normal velocity components on the horizontal and vertical surfaces.
Author: Gaynor J. Adams
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 40
Get Book Here
Book Description
The coefficients of damping in roll and rolling effectiveness (with differential incidence of the horizontal surfaces) are determined for a slender, equal-span, cruciform wing. It is found that the coefficient of damping in ar roll is 62 percent greater than for a plane slender wing of equal aspect ratio, and that the rolling effectiveness is 53 percent less than for a plane slender wing of equal aspect ratio. The analysis can be used in the estimation of the characteristics of a slender, equal-span, cruciform wing having any specified distribution of normal velocity components on the horizontal and vertical surfaces.
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1200
Get Book Here
Book Description
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 54
Get Book Here
Book Description
Author: G. N. Ward
Publisher: Cambridge University Press
ISBN: 1316601897
Category : Mathematics
Languages : en
Pages : 261
Get Book Here
Book Description
Originally published in 1955, this book is devoted exclusively to the problems involved in solving the non-linear equations of motion for compressible fluids.
Author:
Publisher: CUP Archive
ISBN:
Category :
Languages : en
Pages : 268
Get Book Here
Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 654
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 750
Get Book Here
Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 388
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1500
Get Book Here
Book Description
Author: Richard C. Dingeldein
Publisher:
ISBN:
Category : Rotors (Helicopters)
Languages : en
Pages : 650
Get Book Here
Book Description
The power requirements measured in static thrust and in level forward flight are presented for two helicopter rotor configurations. One is a coaxial rotor arrangement having the rotors spaced approximately 19 percent of the rotor radius; the other is a tandem configuration in which the rotor-shaft spacing is 3 percent greater than the rotor daimater and in which the rotors lie in the same plane. The experimental meausrements are compared with the results of calculations based on existing NACA single-rotor theory.
