| Type of Document |
Master's Thesis |
| Author |
Wang, Yu
|
| Author's Email Address |
wangyu@vt.edu |
| URN |
etd-04052000-14200057 |
| Title |
Tip Leakage Flow Downstream a Compressor Cascade with Moving End Wall |
| Degree |
Master of Science |
| Department |
Aerospace and Ocean Engineering |
| Advisory Committee |
| Advisor Name |
Title |
| Devenport, William J. |
Committee Chair |
| Schetz, Joseph A. |
Committee Member |
| Simpson, Roger L. |
Committee Member |
|
| Keywords |
-
- Moving Wall
- Linear Cascade
- Tip leakage Flow
|
| Date of Defense |
2000-03-23 |
| Availability |
unrestricted |
Abstract
A large-scale moving end-wall system has been designed and built at the Aerospace and Ocean Engineering Department of Virginia Tech. This system forms part of a low-speed linear compressor cascade wind tunnel, where it is used to simulate the effects of the relative motion between the blade tips and casing upon the flow. Detailed 4-sensor hot wire measurements were made at various locations downstream the cascade. The results are presented in term of mean flow field and turbulence flow field. In order to reveal the effects of moving end wall, the results also compared with the results obtained with stationary end wall.
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56K Modem |
ISDN (64 Kb) |
ISDN (128 Kb) |
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vita.pdf |
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wy_thesis.pdf |
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