Abstract
Numerical modeling of the three-dimensional flows in a spiral casing of a hydraulic turbine, containing a passage of 360- degree turning and multiple elements of airfoils (the so-called distributor), is made. The physical model is based on a novel two-level approach, comprising of (1) a global model that adequately accounts for the geometry of the spiral casing but smears out the details of the distributor and represents the multiple airfoils by a porous medium treatment, and (2) a local model that performs detailed analysis of flow in the distributor region. The global analysis supplies the inlet flow condition for the individual cascade of distributor airfoils, while the distributor analysis yields the information needed for modeling the characteristics of the porous medium. Comparisons of pressure and velocity profiles between measurement and prediction have been made to assess the validity of the present approach. Flow characteristics in the spiral casing are also discussed.
| Original language | English |
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| Title of host publication | Aircraft Engine; Marine; Microturbines and Small Turbomachinery |
| Publisher | American Society of Mechanical Engineers (ASME) |
| ISBN (Electronic) | 9780791878996 |
| DOIs | |
| Publication status | Published - 1991 |
| Externally published | Yes |
| Event | ASME 1991 International Gas Turbine and Aeroengine Congress and Exposition, GT 1991 - Orlando, United States Duration: 3 Jun 1991 → 6 Jun 1991 |
Publication series
| Name | Proceedings of the ASME Turbo Expo |
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| Volume | 2 |
Conference
| Conference | ASME 1991 International Gas Turbine and Aeroengine Congress and Exposition, GT 1991 |
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| Country/Territory | United States |
| City | Orlando |
| Period | 3/06/91 → 6/06/91 |
Bibliographical note
Publisher Copyright:Copyright © 1991 by ASME.