Hostname: page-component-cd9895bd7-gvvz8 Total loading time: 0 Render date: 2024-12-26T18:06:37.933Z Has data issue: false hasContentIssue false
  • English
  • Français

Notes on the Mean Aerodynamic Chord and the Mean Aerodynamic Centre of a Wing

Published online by Cambridge University Press:  28 July 2016

A. H. Yates
Get access Rights & Permissions [Opens in a new window]

Summary

The relations between the various reference chords used in reports on the loading of wings (standard mean chord, mean aerodynamic chord, centroid of area chord, and so on) are reviewed. Formulae are given for the position on these reference chords of the mean aerodynamic centre of certain simple “ additional” load distributions. References to convenient methods of calculating the load distribution on an arbitrary wing are also given.

Type
Research Article
Information
The Aeronautical Journal , Volume 56 , Issue 498 , June 1952 , pp. 461 - 474
Copyright
Copyright © Royal Aeronautical Society 1952

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

References

Aerodynamic Centre

1. Falkner, V. M. (1944). Preliminary Notes on Aerodynamic Centres of Swept Back Wings. N.P.L. Note, 1944 (unpublished).Google Scholar
2. Falkner, V. M. (1944). Further Notes on Aerodynamic Centres of Swept Back Wings. N.P.L. Note, 1944 (unpublished).Google Scholar
3. Falkner, V. M. Notes on Aerodynamic Centres (unpublished).Google Scholar
4. Weissinger, J. (1947). The Lift Distribution of Swept Back Wings. N.A.C.A. Technical Memorandum 1120, 1947.Google Scholar
5. Schrenk, O. (1940). A Simple Approximate Method for Obtaining the Spanwise Lift Distribution. N.A.C.A. Technical Memorandum 948, 1940. Journal of the Royal Aeronautical Society, October 1941.Google Scholar
6. Van Dorn, N. H. and De Young, J. (1947). A Comparison of Three Theoretical Methods of Calculating Span Load Distribution on Swept Wings. N.A.C.A. Technical Note 1476, 1947.Google Scholar
7. De Young, J. and Harper, C. W. (1948). Theoretical Symmetric Span Loading at Subsonic Speeds for Wings having Arbitrary Plan Form. N.A.C.A. Report 921, 1948.Google Scholar
8. Diederich, F. W. (1948). A Simple Approximate Method for Obtaining Spanwise Lift Distributions over Swept Wings. N.A.C.A. R.M. L7I07, 1948.Google Scholar
9. Stevens, V. I. (1948). Theoretical Basic Span Loading Characteristics of Wings with Arbitrary Sweep, Aspect Ratio and Taper Ratio. N.A.C.A. Technical Note 1772, 1948.Google Scholar
10. Stanton-Jones, R. (1950). A Rapid Method of Estimating the Basic Loading Distribution due to a Linear Twist on Wings of any Plan Form. Saunders-Roe Report A.S.R.7, 1950.Google Scholar
11. De Young, J. (1947). Theoretical Additional Span Loading Characteristics of Wings of Arbitrary Sweep, Aspect Ratio and Taper Ratio. N.A.C.A. Technical Note 1491, 1947.Google Scholar
12. Stanton-Jones, R. (1950). An Empirical Method for Rapidly Determining the Loading Distributions on Swept Back Wings. College of Aeronautics Report No. 32, 1950.Google Scholar