Abstract
The detailed three-dimensional velocity distributions, corresponding to design and off-design operation, were measured in two different circumferential cross sections of a volute by means of LDV. It is shown that the swirl has a forced vortex type velocity distribution and that the location of the swirl center is changing with mass flow. The through flow velocity distribution is primarily defined by the conservation of angular momentum. A strong interaction between the through flow and swirl velocity is observed. Flow visualisation in the tongue region reveals a reversal of the velocity at the volute inlet with increasing mass flow. The pressure drop between volute outlet and inlet at low mass flow pushes extra fluid through the tongue gap and increases the mass flow in the volute. The abrupt pressure rise at high mass flow results in local return flow perturbing the flow in the outlet pipe.
Original language | English |
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Title of host publication | Turbomachinery |
Publisher | American Society of Mechanical Engineers (ASME) |
ISBN (Electronic) | 9780791879047 |
DOIs | |
Publication status | Published - 1990 |
Externally published | Yes |
Event | ASME 1990 International Gas Turbine and Aeroengine Congress and Exposition, GT 1990 - Brussels, Belgium Duration: 11 Jun 1990 → 14 Jun 1990 |
Publication series
Name | Proceedings of the ASME Turbo Expo |
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Volume | 1 |
Conference
Conference | ASME 1990 International Gas Turbine and Aeroengine Congress and Exposition, GT 1990 |
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Country/Territory | Belgium |
City | Brussels |
Period | 11/06/90 → 14/06/90 |
Bibliographical note
Publisher Copyright:© Copyright 1990 by ASME.