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On the theory of a cascade of stalled aerofoils

Published online by Cambridge University Press:  09 April 2009

L. C. Woods
Affiliation:
The University of New South Wales, Sydney.
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Summary

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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
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). 367386.Google Scholar
[8]Woods, L. C., Proc. Roy. Soc. A, 228, (1955b). 5065.Google Scholar
[9]Woods, L. C., Proc. Roy. Soc. A, 238, (1956). 358388.Google Scholar
[10]Woods, L. C., Proc. Roy. Soc. A, 239, (1957). 328337.Google Scholar