Measurement of tip-clearance flow in a multi-stage, axial flow compressor
- 著者名:
- Foley, Andrew C. ( Cranfield University )
- Ivey, Paul C.
- 掲載資料名:
- A.S.M.E. paper
- シリーズ名:
- ASME Technical Paper : GT
- 発行年:
- 1994
- 通号:
- 94-GT-431
- ペーパー番号:
- 94-GT-431
- 出版情報:
- New York: The American Society of Mechanical Engineers
- 言語:
- 英語
- 請求記号:
- A11800
- 資料種別:
- テクニカルペーパー
類似資料:
1
テクニカルペーパー
3D laser transit measurements of the tip clearance vortex in a compressor rotor blade row
The American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
The American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
The American Society of Mechanical Engineers |
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Adminstration |
10
テクニカルペーパー
Effect of axially non-uniform rotor tip clearance on the performance of a high speed axial flow compressor stage
The American Society of Mechanical Engineers |
American Institute of Aeronautics and Astronautics |
11
テクニカルペーパー
The Measurement of Turbomachinery Blade Vibration Through Tip Timing with Capacitance Tip Clearance Probes.
American Society of Mechanical Engineers |
The American Society of Mechanical Engineers |
12
テクニカルペーパー
Tip clearance flow induced endwall boundary layer separation in a single-stage axial-flow low-speed compressor
American Society of Mechanical Engineers |