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Experiments on the low-speed flow past cones

Published online by Cambridge University Press:  28 March 2006

J. R. Calvert
J. R. Calvert
Affiliation:
Engineering Department, University of Cambridge
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Abstract

The wake behind a cone in incompressible flow has the form of a closed bubble. Measurements of velocity, turbulence and static pressure for various cone angles show that the wakes are all essentially similar. A wake Strouhal number may be defined, which is the same for all the models. A disk may be treated as a cone of 180° vertex angle.

Information

Type
Research Article
Information
Journal of Fluid Mechanics , Volume 27 , Issue 2 , 2 February 1967 , pp. 273 - 289
Copyright
© 1967 Cambridge University Press

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References

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Roshko, A. & Lau, J. C. 1965 GALCIT Pasadena publication no. 605. Proc. 1965 Heat Trans. and Fluid Mech. Inst. Stanford University Press.
Stanton, T. E. & Marshall, D. 1932 Aero. Res. Coun. R & M no. 1358.