Experimental study for multi-lobed mixer highbypass exhaust systems for a subsonic jet noise reduction, Part 1. Laser Doppler anemometer results

Experimental study for multi-lobed mixer highbypass exhaust systems for a subsonic jet noise reduction, Part 1. Laser Doppler anemometer results

著者名:

Shin, Hyoun-Woo ( GE Aircraft Engines )

掲載資料名:

5th AIAA/CEAS Aeroacoustics Conference and Exhibit, Bellevue (Greater Seattle), Washington 10-12 May 1999 : a collection of technical papers

シリーズ名:

AIAA Paper : AIAA/CEAS Aeroacoustics Conference

シリーズ巻号:

1999

発行年:

1999

巻:

v. 2

通号:

99-1987

ペーパー番号:

AIAA 99-1987

開始ページ:

1221

出版情報:

Reston, VA: American Institute of Aeronautics and Astronautics

ISBN:

9781563472947 [1563472945]

言語:

英語

請求記号:

A07400/991805

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00006872
シリーズID:	PA00000149
会議名:	AIAA/CEAS Aeroacoustics Conference and Exhibit
回次:	5th
会議開催地:	Bellevue (Greater Seattle), Washington
会議開催年:	1999.05.10-1999.05.12

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1 テクニカルペーパー Experimental study for multi-lobed mixer highbypass exhaust systems for a subsonic jet noise reduction, Part 2: Acoustic results Salikuddin, M., Martens, S., Janardan, B.A., Shin, H., Majjigi, R.K. American Institute of Aeronautics and Astronautics	7 テクニカルペーパー Boundary layer development in axial compressors and turbines part 2 of 4: Compressors Halstead, David E., Walker, Gregory J., Wisler, David C., Hodson, Howard P., Okiishi, Theodore H., Shin, Hyoun-Woo The American Society of Mechanical Engineers
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