Please use this identifier to cite or link to this item: http://hdl.handle.net/2381/22152
Title: POSSIBLE EXTENSION OF PRE-STALL LIMITS FOR FLOWS IN A COMPRESSOR AEROFOIL BLADE ROW BY FRACTAL COMPATIBILITY WITH TOPOGRAPHY IN A FEEDBACK CHANNEL
Authors: THORNTON, BS
BOTTEN, LC
GOSTELOW, JP
First Published: 3-Jun-1991
Publisher: ELSEVIER SCIENCE BV
Citation: PHYSICS LETTERS A, 1991, 156 (1-2), pp. 33-36
DOI Link: 10.1016/0375-9601(91)90122-O
ISSN: 0375-9601
Links: http://hdl.handle.net/2381/22152
Type: Journal Article
Appears in Collections:Published Articles, Dept. of Engineering

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