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A rapid implicit-explicit solution to the two-dimensional time dependent incompressible Navier-Stokes equationsA second-order time-accurate and spatially factored algorithm was used in a finite difference scheme for the numerical solution of the time-dependent, incompressible, two dimensional Navier-Stokes equations in conservation-law form using vorticity and stream function variables. The systems of equations are solved at each time step by an iterative technique. Numerical results were obtained for a circular cylinder at a Reynolds number of 15, and an NACA 0012 airfoil at zero angle of attack at Reynolds numbers of 10 to the third and 10 to the fourth powers. The results are in agreement with another numerical technique, and the computing time required to obtain the steady state solution at the Reynolds number of 10 to the 4th power was 49.7 sec on CDC 7600 computer using a 65 x 84 computational grind.
Document ID
19800025210
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Davis, J. E.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 4, 2013
Publication Date
October 1, 1980
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CR-3330
Report Number: NASA-CR-3330
Accession Number
80N33718
Funding Number(s)
CONTRACT_GRANT: NASA ORDER A-50807-B
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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