Influence of Moving End-wall on Tip Clearance Flow in Axial Compressor Cascades
- 著者名:
- 掲載資料名:
- AIAA meeting papers on disc
- シリーズ名:
- AIAA Paper : Aerospace Sciences Meeting and Exhibit
- シリーズ巻号:
- 2006
- 発行年:
- 2006
- 通号:
- 2006-0630
- ペーパー番号:
- AIAA Paper 2006-630
- 出版情報:
- Reston, Va.: American Institute of Aeronautics and Astronautics
- ISSN:
- 10877215
- 言語:
- 英語
- 請求記号:
- A07400/200603 [CD-ROM 2006 Disc 3]
- 資料種別:
- テクニカルペーパー
類似資料:
American Institute of Aeronautics and Astronautics |
The American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
American Institute of Aeronautics and Astronautics |
3
テクニカルペーパー
Mechanism of the Interaction Between Casing Treatment and Tip Leakage Flow in a Subsonic Axial Compressor.
American Society of Mechanical Engineers |
National Aeronautics and Space Adminstration |
American Society of Mechanical Engineers |
10
テクニカルペーパー
Experimental Study of Tip Leakage Flow in the Linear Compressor Cascade: Part II - Effect of Moving Wall
American Institute of Aeronautics and Astronautics |
American Society of Mechanical Engineers |
11
テクニカルペーパー
Unsteady Tip Clearance Flow in a Low-Speed Axial Compressor Rotor with Upstream and Downstream Stators.
American Society of Mechanical Engineers |
American Institute of Aeronautics and Astronautics |
12
テクニカルペーパー
The Effects of Stepped Tip Gap on Performance and Flowfield of a Subsonic Axial-Flow Compressor Rotor.
American Society of Mechanical Engineers |