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Improved numerical methods for turbulent viscous flows aerothermal modeling program, phase 2The details of a study to develop accurate and efficient numerical schemes to predict complex flows are described. In this program, several discretization schemes were evaluated using simple test cases. This assessment led to the selection of three schemes for an in-depth evaluation based on two-dimensional flows. The scheme with the superior overall performance was incorporated in a computer program for three-dimensional flows. To improve the computational efficiency, the selected discretization scheme was combined with a direct solution approach in which the fluid flow equations are solved simultaneously rather than sequentially.
Document ID
19890002639
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Karki, K. C.
(Detroit Diesel Allison Indianapolis, IN, United States)
Patankar, S. V.
(Detroit Diesel Allison Indianapolis, IN, United States)
Runchal, A. K.
(Detroit Diesel Allison Indianapolis, IN, United States)
Mongia, H. C.
(Detroit Diesel Allison Indianapolis, IN, United States)
Date Acquired
September 5, 2013
Publication Date
June 1, 1988
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CR-182169
NAS 1.26:182169
EDR-13519
Report Number: NASA-CR-182169
Report Number: NAS 1.26:182169
Report Number: EDR-13519
Accession Number
89N12010
Funding Number(s)
CONTRACT_GRANT: NAS3-24350
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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