Effect of Circumferential Grooves on the Aerodynamic Performance of an Axial Single-Stage Transonic Compressor
- 著者名:
- 掲載資料名:
- ASME Turbo Expo 2007: Power for Land, Sea, and Air (GT2007)
- シリーズ名:
- ASME Symposia Volumes
- シリーズ巻号:
- TURBO EXPO 2007(6A)
- 発行年:
- 2007
- 巻:
- 6A
- ペーパー番号:
- GT2007-27365
- 開始ページ:
- 115
- 終了ページ:
- 124
- 総ページ数:
- 10
- 出版情報:
- New York: American Society of Mechanical Engineers
- ISBN:
- 9780791847954 [0791847950]
- 言語:
- 英語
- 請求記号:
- A11661/2007
- 資料種別:
- 国際会議録
類似資料:
American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
4
国際会議録
Short Length-Scale Rotating Stall Inception in a Transonic Axial Compressor: Criteria and Mechanisms
American Society of Mechanical Engineers |
10
テクニカルペーパー
Unsteady Pressure Measurement in a Single Stage Axial Transonic Compressor Near the Stability Limit.
American Society of Mechanical Engineers |
5
国際会議録
Unsteady Pressure Measurement in a Single Stage Axial Transonic Compressor Near the Stability Limit
American Society of Mechanical Engineers |
11
テクニカルペーパー
Development of hub corner stall and its influence on the performance of axial compressor blade rows
The American Society of Mechanical Engineers |
American Society of Mechanical Engineers |
The American Society of Mechanical Engineers |