[PDF] Analysis Of Available Data On The Effects Of Tabs On Control Surface Hinge Moments eBook

Analysis Of Available Data On The Effects Of Tabs On Control Surface Hinge Moments Book in PDF, ePub and Kindle version is available to download in english. Read online anytime anywhere directly from your device. Click on the download button below to get a free pdf file of Analysis Of Available Data On The Effects Of Tabs On Control Surface Hinge Moments book. This book definitely worth reading, it is an incredibly well-written.

Analysis of Available Data on the Effects of Tabs on Control-surface Hinge Moments

Author : Stewart M. Crandall
Publisher :
Page : 28 pages
File Size : 43,9 MB
Release : 1946
Category : Airplanes
ISBN :

GET BOOK

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.

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

Author : Paul E. Purser
Publisher :
Page : 570 pages
File Size : 14,18 MB
Release : 1947
Category : Aerofoils
ISBN :

GET BOOK

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.

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

Author : Paul E. Purser
Publisher :
Page : 34 pages
File Size : 22,7 MB
Release : 1947
Category : Aerofoils
ISBN :

GET BOOK

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.

Performance Tests of Wire Strain Gages

Author : William R. Campbell
Publisher :
Page : 606 pages
File Size : 18,18 MB
Release : 1946
Category : Aeronautics
ISBN :

GET BOOK

Results of calibrations to determine axial and transverse strain sensitivities are presented for 15 types of single-element, multistrand wire strain gage.

Stability and Control

Author : Courtland D. Perkins
Publisher : Elsevier
Page : 520 pages
File Size : 39,56 MB
Release : 2014-05-12
Category : Technology & Engineering
ISBN : 1483222330

GET BOOK

Flight Testing, Volume II: Stability and Control focuses on the development of adequate flight test techniques for the appraisal of stability and control characteristics and flying qualities of airplanes. This book discusses the flying quality requirements, longitudinal motions, and flight determination of stick-fixed neutral points. The determination of aerodynamic parameters from steady maneuvering, desirable control characteristics in steady flight, and various forms of lateral control surfaces are also elaborated. This publication likewise covers the measurement of maximum lift coefficient, emergency anti-spin devices, and concept of the altitude-Mach number flight envelope. This volume is recommended for design, development or research engineers, test pilots, and instrumentation personnel interested in airplane stability and control.

Index of NACA Technical Publications

Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 306 pages
File Size : 13,78 MB
Release : 1956
Category : Aeronautics
ISBN :

GET BOOK

Technical Note

Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 494 pages
File Size : 23,4 MB
Release : 1947
Category : Aeronautics
ISBN :

GET BOOK

Structural Loads Analysis

Author : Ted L. Lomax
Publisher : AIAA
Page : 306 pages
File Size : 35,9 MB
Release : 1996
Category : Airframes
ISBN : 9781600861185

GET BOOK