Closed-loop separation control using oscillatory flow excitation [microform] / Brian G. Allan [and others] ; [prepared for ... under contract NAS1-97046]

"Design and implementation of a digital feedback controller for a flow control experiment was performed. The experiment was conducted in a cryogenic pressurized wind tunnel on a generic separated configuration at a chord Reynolds number of 16 million and a Mach number of 0.25. The model simulat...

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Bibliographic Details
Corporate Author: Institute for Computer Applications in Science and Engineering
Other Authors: Allan, Brian G.
Format: Government Document Microfilm Book
Language:English
Published: Hampton, Va. : Hanover, MD : ICASE, National Aeronautics and Science Administration, Langley Research Center ; Available from NASA Center for Aerospace Information, [2000]
Series:NASA contractor report ; NASA CR-210324.
ICASE report ; no. 2000-32.
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Norlin Library - Government Information - Microform

Holdings details from Norlin Library - Government Information - Microform
Call Number: NAS 1.26:210324
NAS 1.26:210324 Restricted Place a Hold