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A Navier-Stokes Solution of Hull-Ring Wing-Thruster InteractionNavier-Stokes simulations of high Reynolds number flow around an axisymmetric body supported in a water tunnel were made. The numerical method is based on a finite-differencing high resolution second-order accurate implicit upwind scheme. Four different configurations were investigated, these are: (1) barebody; (2) body with an operating propeller; (3) body with a ring wing; and (4) body with a ring wing and an operating propeller. Pressure and velocity components near the stern region were obtained computationally and are shown to compare favorably with the experimental data. The method correctly predicts the existence and extent of stern flow separation for the barebody and the absence of flow separation for the three other configurations with ring wing and/or propeller.
Document ID
19920005092
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Yang, C.-I.
(David Taylor Research Center Bethesda, MD., United States)
Hartwich, P.
(NASA Langley Research Center Hampton, VA, United States)
Sundaram, P.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1991
Publication Information
Publication: NAS-NRC, Eighteenth Symposium on Naval Hydrodynamics
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
92N14310
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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