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A vortex wake capturing method for potential flow calculationsA method is presented for modifying finite difference solutions of the potential equation to include the calculation of non-planar vortex wake features. The approach is an adaptation of Baker's 'cloud in cell' algorithm developed for the stream function-vorticity equations. The vortex wake is tracked in a Lagrangian frame of reference as a group of discrete vortex filaments. These are distributed to the Eulerian mesh system on which the velocity is calculated by a finite difference solution of the potential equation. An artificial viscosity introduced by the finite difference equations removes the singular nature of the vortex filaments. Computed examples are given for the two-dimensional time dependent roll-up of vortex wakes generated by wings with different spanwise loading distributions.
Document ID
19820048394
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Murman, E. M.
(MIT Cambridge, MA, United States)
Stremel, P. M.
(NASA Ames Research Center Moffett Field, CA; MIT, Cambridge, MA, United States)
Date Acquired
August 10, 2013
Publication Date
June 1, 1982
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 82-0947
Meeting Information
Meeting: Joint Thermophysics, Fluids, Plasma and Heat Transfer Conference
Location: St. Louis, MO
Start Date: June 7, 1982
End Date: June 11, 1982
Sponsors: American Institute of Aeronautics and Astronautics and American Society of Mechanical Engineers
Accession Number
82A31929
Funding Number(s)
CONTRACT_GRANT: NAG2-105
Distribution Limits
Public
Copyright
Other

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