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three-dimensional flow field measurements in a radial inflow turbine scroll using ldvThe results of an experimental study of the three-dimensional flow field in a radial inflow turbine scroll are presented. A two-color LDV system was used in the measurement of three orthogonal velocity components at 758 points located throughout the scroll and the unvaned portion of the nozzle. The cold flow experimental results are presented for through-flow velocity contours and the cross velocity vectors.
Document ID
19860063443
Document Type
Conference Paper
Authors
Malak, M. F.
(Cincinnati Univ. OH, United States)
Hamed, A.
(Cincinnati Univ. OH, United States)
Tabakoff, W.
(Cincinnati, University OH, United States)
Date Acquired
August 12, 2013
Publication Date
June 1, 1986
Subject Category
AERODYNAMICS
Report/Patent Number
ASME PAPER 86-GT-122
Funding Number(s)
CONTRACT_GRANT: NAG3-26
Distribution Limits
Public
Copyright
Other