[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 : 14,21 MB
Release : 1947
Category : Aerofoils
ISBN :

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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 : 41,20 MB
Release : 1946
Category : Airplanes
ISBN :

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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

Author :
Publisher :
Page : 630 pages
File Size : 47,55 MB
Release : 1947
Category : Aeronautics
ISBN :

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Collection and Analysis of Hinge-moment Data on Control-surface Tabs

Author : Paul E. Purser
Publisher :
Page : 570 pages
File Size : 36,5 MB
Release : 1947
Category : Aerofoils
ISBN :

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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 : 39,55 MB
Release : 1960
Category : Aeronautics
ISBN :

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Includes its Reports, which are also issued separately.

Annual Report of the National Advisory Committee for Aeronautics

Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 988 pages
File Size : 27,83 MB
Release : 1950
Category : Aeronautics
ISBN :

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Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.