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Analysis of the three dimensional flow in a turbine scrollThe present analysis describes the three-dimensional compressible inviscid flow in the scroll and the vaneless nozzle of a radial inflow turbine. The solution to this flow field, which is further complicated by the geometrical shape of the boundaries, is obtained using the finite element method. Symmetric and nonsymmetric scroll cross sectional geometries are investigated to determine their effect on the general flow field and on the exit flow conditions.
Document ID
19800043571
Document Type
Conference Proceedings
Authors
Hamed, A. (Cincinnati Univ. OH, United States)
Baskharone, E. (Cincinnati, University Cincinnati, Ohio, United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1979
Subject Category
AERODYNAMICS
Meeting Information
Flow in primary, non-rotating passages in turbomachines(New York, NY)
Funding Number(s)
CONTRACT_GRANT: NSG-3066
Distribution Limits
Public
Copyright
Other