Hostname: page-component-586b7cd67f-t8hqh Total loading time: 0 Render date: 2024-11-22T06:36:43.047Z Has data issue: false hasContentIssue false
  • English
  • Français

On the theory of a cascade of stalled aerofoils

Published online by Cambridge University Press:  09 April 2009

L. C. Woods
L. C. Woods
Affiliation:
The University of New South Wales, Sydney.
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 of the separating flow past a cascade of aerofoils is developed. The flow is assumed to be inviscid, incompressible and twodimensional. The wakes are represented by regions of stationary fluid, which could, in the general case, maintain a pressure gradient, although much of the theory is developed for the case of constant wake pressure.

Type
Research Article
Information
Journal of the Australian Mathematical Society , Volume 1 , Issue 2 , February 1960 , pp. 210 - 219
Copyright
Copyright © Australian Mathematical Society 1960

References

[1]Birkhoff, G. and Zarantonello, E. H., Jets, Wakes and Cavities. Academic Press, New York. (1957).Google Scholar
[2]Chang, C. C. and Chu, V. C., J. Appl. Mech. (1956).Google Scholar
[3]Kemp, H. N. and Sears, W. R., J. Aero. Sci. (9), 20, (1953). 585.CrossRefGoogle Scholar
[4]Pearson, H., Proc. 4th Anglo-American Aero. Conference (R. Ae. S.), (1953). 127–162.Google Scholar
[5]Robinson, A. and Laurmann, J. A., Wing Theory, Camb. Univ. Press. (1956).Google Scholar
[6]Rosenblat, S. and Woods, L. C., Aust. Aero. Res. Comm. Report ACA-58. (1956).Google Scholar
[7]Woods, L. C., Proc. Roy. Soc. A, 227, (1955a). 367–386.Google Scholar
[8]Woods, L. C., Proc. Roy. Soc. A, 228, (1955b). 50–65.Google Scholar
[9]Woods, L. C., Proc. Roy. Soc. A, 238, (1956). 358–388.Google Scholar
[10]Woods, L. C., Proc. Roy. Soc. A, 239, (1957). 328–337.Google Scholar