Using some simple assumptions with regard to the boundary conditions and confining the considerations to flows with small Rossby numbers, a pattern of streamlines corresponding to an axial plane of an incompressible vortex flow in a cylindrical vortex chamber is computed. The pattern obtained agrees qualitatively, in the main regions, with velocity profile measurements and dye-injection flow visualization experiments.
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References
1.
KotasT. J.Le FevreE. J.‘An optical technique for measuring the velocity of a fluid’, J. mech. Engng Sci.197517 (April), 65–70.
2.
KotasT. J.‘Turbulent boundary layer flow on the end wall of a cylindrical vortex chamber’, Proc. Instn mech. Engrs1975189, 305–315.
3.
KotasT. J.‘An experimental study of the three-dimensional boundary layer on the end wall of a cylindrical vortex chamber’. Proc. R. Soc. A1976352 (December), 169–187.
4.
RosenzweigM. L.RossD. H.LewellenW. S.‘On secondary flows in jet-driven vortex tubes’, J. Aero Space Sci.1962 (September), 1142.
MackL. M.The laminar boundary layer on a disc of a finite radius in a rotating flow, Part 1 Jet Propulsion Laboratory TR No. 32–224.
8.
KotasT. J.An experimental study of a confined vortex flow Faculty of Engineering Report No. QMC-EP 5007, Queen Mary College, London, July 1975.
9.
KotasT. J.A solution for the turbulent boundary layer on the end wall of a vortex chamber Faculty of Engineering Report No. QMC-EP 5008, Queen Mary College, London, July 1975.