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The Influence of Attached Boundary Layers in Determining the Optimum for Blades in Cascade

Published online by Cambridge University Press:  04 July 2016

W. K. Allan  and
B. S. Stratford
W. K. Allan
Affiliation:
Dept. of Mechanical Engineering, University College, London
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Extract

Dr. Stratford (p. 133, February 1965 Journal) is to be supported in his endeavour to apply boundary layer theory to the prediction of optimum loading requirements in flow through blades in cascade. Inevitably some simplification of the general flow system in a blade passage is necessary if undue complexity is to be avoided. In the simplified flow model, however, care must be taken to avoid over-simplification, and the limitations imposed by legitimate approximations must be appreciated.

Type
Technical Notes
Information
The Aeronautical Journal , Volume 69 , Issue 655 , July 1965 , pp. 497 - 498
Copyright
Copyright © Royal Aeronautical Society 1965

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References

1.Smith, S. F. A Simple Correlation of Turbine Efficiency. Seminar on Advanced Problems in Turbomachinery, at the von Karman Institute for Fluid Dynamics, March 1965.Google Scholar