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A Moving Grid Capability for NPARCVersion 3.1 of the NPARC computational fluid dynamics flow solver introduces a capability to solve unsteady flow on moving multi-block, structured grids with nominally second-order time accuracy. The grid motion is due to segments of the boundary grid that translate and rotate in a rigid-body manner or deform. The grid is regenerated at each time step to accommodate the boundary grid motion. The flow equations and computational models sense the moving grid through the grid velocities, which are computed from a time-difference of the grids at two consecutive time levels. For three-dimensional flow domains, it is assumed that the grid retains a planar character with respect to one coordinate. The application and accuracy of NPARC v3.1 is demonstrated for flow about a flying wedge, rotating flap, a collapsing bump in a duct, and the upstart / restart flow in a variable-geometry inlet. The results compare well with analytic and experimental results.
Document ID
19980206747
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Slater, John W.
(NASA Lewis Research Center Cleveland, OH United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1998
Subject Category
Aeronautics (General)
Report/Patent Number
NAS 1.15:207944
E-11223
AIAA Paper 98-0955
NASA/TM-1998-207944
Report Number: NAS 1.15:207944
Report Number: E-11223
Report Number: AIAA Paper 98-0955
Report Number: NASA/TM-1998-207944
Meeting Information
Meeting: Aerospace Sciences Meeting and Exhibit
Location: Reno, NV
Country: United States
Start Date: January 12, 1998
End Date: January 15, 1998
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
PROJECT: RTOP 509-10-51
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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