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Two-Dimensional Computational Model for Wave Rotor Flow DynamicsA two-dimensional (theta,z) Navier-Stokes solver for multi-port wave rotor flow simulation is described. The finite-volume form of the unsteady thin-layer Navier-Stokes equations are integrated in time on multi-block grids that represent the stationary inlet and outlet ports and the moving rotor passages of the wave rotor. Computed results are compared with three-port wave rotor experimental data. The model is applied to predict the performance of a planned four-port wave rotor experiment. Two-dimensional flow features that reduce machine performance and influence rotor blade and duct wall thermal loads are identified. The performance impact of rounding the inlet port wall, to inhibit separation during passage gradual opening, is assessed.
Document ID
19960017557
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Welch, Gerard E.
(Army Research Lab. Cleveland, OH United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1996
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
ARL-TR-924
NAS 1.15:107192
NASA-TM-107192
E-10164
Report Number: ARL-TR-924
Report Number: NAS 1.15:107192
Report Number: NASA-TM-107192
Report Number: E-10164
Meeting Information
Meeting: Turbo Expo 1996
Location: Birmingham
Country: United Kingdom
Start Date: June 10, 1996
End Date: June 13, 1996
Sponsors: American Society of Mechanical Engineers
Accession Number
96N23138
Funding Number(s)
PROJECT: RTOP 505-62-75
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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