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Screened Expanding Turning Vane Concept

Author(s)
Drela, Mark; Huang, Arthur C.; Darmofal, David L
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Abstract
The paper presents the screened expanding corner vane concept, which can turn a channel flow by 90 degrees, while simultaneously increasing the flow area by at least a factor of two and thus halving the mean velocity, all without incurring any significant flow separation. The concept is demonstrated experimentally, and investigated with analytical and computational models. One target application is an ultra-compact closed-circuit wind tunnel, whose overall length is less than half of a conventional wind tunnel with the same test section.
Date issued
2019-01
URI
https://hdl.handle.net/1721.1/123882
Department
Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
Journal
AIAA Scitech 2019 Forum
Publisher
American Institute of Aeronautics and Astronautics
Citation
Drela, Mark et al. "Screening Expanding Turning Vane Concept." AIAA Scitech 2019 Forum. January 2019, San Diego, California, AIAA Scitech 2019 Forum, January 2019 © 2019 The Author(s)
Version: Author's final manuscript
ISBN
9781624105784

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