Aircraft Engine Fault Detection Using Dynamic/Adaptive Threshold Approach.

Aircraft Engine Fault Detection Using Dynamic/Adaptive Threshold Approach.

著者名:

掲載資料名:

A.S.M.E. paper

シリーズ名:

ASME Technical Paper : GT

シリーズ巻号:

2007

発行年:

2007

通号:

GT2007-28180

ペーパー番号:

GT2007-28180

総ページ数:

8

出版情報:

New York, NY: American Society of Mechanical Engineers

言語:

英語

請求記号:

A11800

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00052166
シリーズID:	PA00000136
会議名:	ASME Turbo Expo 2007: Power for Land, Sea and Air
回次:	2007
会議開催地:	Montreal, Canada
会議開催年:	2007.05.14-2007.05.17
論文注記:	ASME Turbo Expo 2007: Power for Land, Sea and Air, Montreal, Canada, 2007.5.14-2007.05.17

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