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Application of radial-splitters for improved wide-angle diffuser performance in a blowdown tunnelSevere flow separation in the 15:1 area-ratio, 38 deg total angle conical diffuser preceding the settling-chamber of an intermittent blowdown wind tunnel was eliminated by the use of a novel radial-splitter arrangement. As a consequence, the operating life of settling-chamber screens was greatly extended and test-section flow steadiness improved, with no penalty in the tunnel running time.
Document ID
19760054308
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Rao, D. M.
(NASA Langley Research Center Hampton, Va.; National Aeronautical Laboratory, Bangalore, India)
Seshadri, S. N.
(National Aeronautical Laboratory Bangalore, India)
Date Acquired
August 8, 2013
Publication Date
July 1, 1976
Publication Information
Publication: Journal of Aircraft
Volume: 13
Subject Category
Aerodynamics
Accession Number
76A37274
Distribution Limits
Public
Copyright
Other

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