Periodical Unsteady Flow Within a Rotor Blade Row of an Axial Compressor: Part II - Wake-Tip Clearance Vortex Interaction
- 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(6B)
- 発行年:
- 2007
- 巻:
- 6B
- ペーパー番号:
- GT2007-27211
- 開始ページ:
- 1587
- 終了ページ:
- 1598
- 総ページ数:
- 12
- 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:
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American Society of Mechanical Engineers |
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テクニカルペーパー
Periodical Unsteady Flow within a Rotor Blade Row of an Axial Compressor: Part I - Flow Field at Midspan.
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The Periodical Interaction of the Tip Clearance Flow in the Blade Rows of Axial Compressors.
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Effect of Clocking on the Unsteady Rotor Blade Loading in a 1.5-Stage Low-Speed Axial Compressor
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Unsteady Aerodynamic Blade Excitation at the Stability Limit and During Rotating Stall in an Axial Compressor.
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Rotating instabilities in an axial compressor originating from the fluctuating blade tip vortex
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