Abstract
This report discusses a cascade wake experiment intended to improve wake modeling in an airfoil analysis. The experiment included extensive measurements of the near and far wakes, trailing edge boundary layers, and airfoil surface static pressures. The measured wake displacement surface and computed boundary layers were used in conjunction with a cascade potential flow solver to demonstrate the feasibility of modeling the viscous aspects of cascade flow.
Original language | English (US) |
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Title of host publication | Turbomachinery |
Publisher | American Society of Mechanical Engineers (ASME) |
ISBN (Electronic) | 9780791879566 |
DOIs | |
State | Published - 1982 |
Externally published | Yes |
Event | ASME 1982 International Gas Turbine Conference and Exhibit, GT 1982 - London, United Kingdom Duration: Apr 18 1982 → Apr 22 1982 |
Publication series
Name | Proceedings of the ASME Turbo Expo |
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Volume | 1 |
Other
Other | ASME 1982 International Gas Turbine Conference and Exhibit, GT 1982 |
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Country/Territory | United Kingdom |
City | London |
Period | 4/18/82 → 4/22/82 |
ASJC Scopus subject areas
- Engineering(all)