Hostname: page-component-7bb8b95d7b-2h6rp Total loading time: 0 Render date: 2024-09-18T18:11:05.923Z Has data issue: false hasContentIssue false
  • English
  • Français

The lifting two-dimensional aerofoil between slotted walls

Published online by Cambridge University Press:  09 April 2009

A. H. Low
A. H. Low
Affiliation:
School of Mathematics, The University of New South Wales, Kensington, N.S.W.
Rights & Permissions [Opens in a new window]

Summary

Core share and HTML view are not available for this content. However, as you have access to this content, a full PDF is available via the ‘Save PDF’ action button.

A mathematical theory is developed which enables the wind-tunnel corrections to the lift and moment forces acting on an aerofoil in subsonic two-dimensional flow to be calculated. The usual “averaged” boundary condition for slotted walls is assumed and the corrections obtained by successive approximation from the open-jet tunnel.

Type
Research Article
Information
Journal of the Australian Mathematical Society , Volume 3 , Issue 2 , May 1963 , pp. 207 - 219
Copyright
Copyright © Australian Mathematical Society 1963

References

[1]Baldwin, B. S., Turner, J. B. and Knechtel, E. D., N.A.C.A. Washington, Tech. Note 3176. (1954).Google Scholar
[2]Byrd, P. F. and Friedmann, M. D., Handbook of Elliptic Integrals (Springer-Verlag, Berlin, 1954).Google Scholar
[3]Low, A. H., Unpublished Ph. D. Thesis, The University of New South Wales (1960).Google Scholar
[4]Low, A. H. and Woods, L. C., J. Austr. Math. Soc., 1 (1960) 220.CrossRefGoogle Scholar
[5]Maeder, P. F. and Wood, A. D., Z.A.M.P. 7 (1956), 177.Google Scholar
[6]Robinson, A. and Laurmann, J. A., Wing Theory (C.U.P., 1956).Google Scholar
[7]Woods, L. C., Quart. J. Mech. and App. Maths. 7 (1954), 263.CrossRefGoogle Scholar
[8]Woods, L. C., Proc. Roy. Soc. A, 229 (1955), 63.Google Scholar
[9]Woods, L. C., Proc. Roy. Soc. A, 229 (1955), 235.Google Scholar
[10]Woods, L. C., Proc. Roy. Soc. A, 242 (1957), 341.Google Scholar
[11]Woods, L. C., Subsonic Plane Flow (C.U.P., 1961).Google Scholar