Numercial Simulation of the Effect of Inlet Distortion to the Subsonic Axial-Flow Compressor

Numercial Simulation of the Effect of Inlet Distortion to the Subsonic Axial-Flow Compressor

著者名:

Y. Zhang ( Northwestern Polytechnical University, Xi'an, Shaanxi, China (prc) )
W. Chu
X. Lu

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:

2008

発行年:

2008

通号:

2008-0077

ペーパー番号:

AIAA Paper 2008-0077

出版情報:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

言語:

英語

請求記号:

A07400/200801 [CD-ROM 2008 Disc 1]

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00049519
シリーズID:	PA00000138
会議名:	AIAA Aerospace Sciences Meeting and Exhibit
回次:	46th
会議開催地:	Reno, Nevada
会議開催年:	2008.01.07-2008.01.10
論文注記:	46th AIAA Aerospace Sciences Meeting and Exhibit, 7-10 January 2008, Reno, Nevada

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1 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. Lu, X., Chu, W., Zhu, J., Wu, Y. American Society of Mechanical Engineers	7 テクニカルペーパー Experimental and Numerical Investigation of a Subsonic Compressor with Bend Skewed Slot Casing Treatment. Lu, X., Chu, W., Zhu, J., Wu, Y. American Society of Mechanical Engineers
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