Theoretical Damping in Roll and Rolling Effectiveness of Slender Cruciform Wings

Theoretical Damping in Roll and Rolling Effectiveness of Slender Cruciform Wings
Author :
Publisher :
Total Pages : 40
Release :
ISBN-13 : UOM:39015086494948
ISBN-10 :
Rating : 4/5 ( Downloads)

Book Synopsis Theoretical Damping in Roll and Rolling Effectiveness of Slender Cruciform Wings by : Gaynor J. Adams

Download or read book Theoretical Damping in Roll and Rolling Effectiveness of Slender Cruciform Wings written by Gaynor J. Adams and published by . This book was released on 1951 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.


Theoretical Damping in Roll and Rolling Effectiveness of Slender Cruciform Wings Related Books

Theoretical Damping in Roll and Rolling Effectiveness of Slender Cruciform Wings
Language: en
Pages: 40
Authors: Gaynor J. Adams
Categories: Airplanes
Type: BOOK - Published: 1951 - Publisher:

DOWNLOAD EBOOK

The coefficients of damping in roll and rolling effectiveness (with differential incidence of the horizontal surfaces) are determined for a slender, equal-span,
Annual Report of the National Advisory Committee for Aeronautics
Language: en
Pages: 1200
Authors: United States. National Advisory Committee for Aeronautics
Categories: Aeronautics
Type: BOOK - Published: 1954 - Publisher:

DOWNLOAD EBOOK

Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
Report
Language: en
Pages: 54
Authors: United States. National Advisory Committee for Aeronautics
Categories: Aeronautics
Type: BOOK - Published: 1956 - Publisher:

DOWNLOAD EBOOK

Linearized Theory of Steady High-Speed Flow
Language: en
Pages: 261
Authors: G. N. Ward
Categories: Mathematics
Type: BOOK - Published: 2016-02-25 - Publisher: Cambridge University Press

DOWNLOAD EBOOK

Originally published in 1955, this book is devoted exclusively to the problems involved in solving the non-linear equations of motion for compressible fluids.
Technical Note - National Advisory Committee for Aeronautics
Language: en
Pages: 654
Authors: United States. National Advisory Committee for Aeronautics
Categories: Aeronautics
Type: BOOK - Published: 1951 - Publisher:

DOWNLOAD EBOOK