Measurement of Unsteady Blade Surface Pressure on a Single Rotation Large Scale Advanced Prop-Fan With Angular and Wake Inflow at Mach Numbers From 0.02 to 0.70

Measurement of Unsteady Blade Surface Pressure on a Single Rotation Large Scale Advanced Prop-Fan With Angular and Wake Inflow at Mach Numbers From 0.02 to 0.70

著者名:

Bushnell, P. ( Hamilton Standard )
Gruber, M.
Parzych, D.

掲載資料名:

NASA Technical Reports

発行年:

1988

号:

NASA-CR-182123

通号:

G3/07 0310411

パート:

NAS 1.26:182123

ペーパー番号:

N91-10065

開始ページ:

1

終了ページ:

45

総ページ数:

45

出版情報:

National Aeronautics and Space Adminstration

言語:

英語

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:	ZA00001427
論文注記:	NAS3-23051

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