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Numerical vorticity capturing for vortex-solid body interaction problemsA new numerical method based on adding a term to the Euler/Navier-Stokes equations has been demonstrated it can effectively treat vortex-dominated flows using low-order numerical schemes and coarse grids. The numerical diffusion introduced by convection schemes can be eliminated by modifying the velocity field as a result of solving the modified flow governing equations. The modification of the velocity field, which conserves the total vorticity, essentially convects the vorticity toward its local extreme to offset the numerical diffusion. This method preserves the vortex structure even when vortices travel on coarse grid region. The method is implemented with two distinctive codes: a Navier-Stokes flow solver based on vorticity-velocity formulation and an Euler code based on velocity-pressure formulation. Problems presented in this paper include airfoil dynamic stall, vortex airfoil interaction, and vortex-fuselage interactions.
Document ID
19930061040
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Wang, Clin M.
(Flow Analysis, Inc. Tullahoma, TN, United States)
Steinhoff, John S.
(NASA Ames Research Center Moffett Field, CA, United States)
Wenren, Yonghu
(UTSI; Flow Analysis, Inc. Tullahoma, TN, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1993
Publication Information
Publication: In: AIAA Computational Fluid Dynamics Conference, 11th, Orlando, FL, July 6-9, 1993, Technical Papers. Pt. 1 (A93-44994 18-34)
Publisher: American Institute of Aeronautics and Astronautics
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 93-3343
Report Number: AIAA PAPER 93-3343
Accession Number
93A45037
Distribution Limits
Public
Copyright
Other

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