Author : D. J. Lyons
Publisher :
Page : 9 pages
File Size : 24,78 MB
Release : 1942
Category :
ISBN :
[PDF] Note On The Analysis Of Experimental Data On The Hinge Moments Of Control Surfaces Due To Tabs eBook
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Collection and Analysis of Hinge-moment Data on Control-surface Tabs
Author : Paul E. Purser
Publisher :
Page : 34 pages
File Size : 46,10 MB
Release : 1947
Category : Aerofoils
ISBN :
Various wind-tunnel data on the hinge-moment characteristics of control-surface tabs have been collected and analyzed. The data, all of which are for plain unbalanced tabs, were obtained from force tests of models in two- and three-dimensional flow and from pressure-distribution measurements on models in two-dimensional flow. Some data that show the effects of Mach number on tab hinge moments for representative conventional and NACA 6-series airfoil sections are presented.
Analysis of Available Data on the Effects of Tabs on Control-surface Hinge Moments
Author : Stewart M. Crandall
Publisher :
Page : 28 pages
File Size : 16,36 MB
Release : 1946
Category : Airplanes
ISBN :
An analysis was made of the hinge-moment effectiveness of tabs based on the available two- and three-dimensional tab data. The results of the analysis indicated that the effects of tabs on control-surface hinge moments can be estimated from geometric characteristics of the tab-flap-airfoil combination with a reasonable degree of accuracy.
Technical Note - National Advisory Committee for Aeronautics
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 1076 pages
File Size : 24,87 MB
Release : 1958
Category : Aeronautics
ISBN :
Technical Note
Author :
Publisher :
Page : 630 pages
File Size : 25,12 MB
Release : 1947
Category : Aeronautics
ISBN :
Collection and Analysis of Hinge-moment Data on Control-surface Tabs
Author : Paul E. Purser
Publisher :
Page : 570 pages
File Size : 39,17 MB
Release : 1947
Category : Aerofoils
ISBN :
Various wind-tunnel data on the hinge-moment characteristics of control-surface tabs have been collected and analyzed. The data, all of which are for plain unbalanced tabs, were obtained from force tests of models in two- and three-dimensional flow and from pressure-distribution measurements on models in two-dimensional flow. Some data that show the effects of Mach number on tab hinge moments for representative conventional and NACA 6-series airfoil sections are presented.
Technical Report
Author : Aeronautical Research Council (Great Britain)
Publisher :
Page : 720 pages
File Size : 14,21 MB
Release : 1960
Category : Aeronautics
ISBN :
Includes its Reports, which are also issued separately.
Note on the Estimation of Control Surface Hinge Moments Due to Tabs
Author : J. G. Walker
Publisher :
Page : 13 pages
File Size : 14,41 MB
Release : 1946
Category :
ISBN :
Journal of the Royal Aeronautical Society
Author :
Publisher :
Page : 954 pages
File Size : 29,79 MB
Release : 1953
Category : Aeronautics
ISBN :
Annual Report of the National Advisory Committee for Aeronautics
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 988 pages
File Size : 10,95 MB
Release : 1950
Category : Aeronautics
ISBN :
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.