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Flowfield-Dependent Mixed Explicit-Implicit (FDMEL) Algorithm for Computational Fluid DynamicsDespite significant achievements in computational fluid dynamics, there still remain many fluid flow phenomena not well understood. For example, the prediction of temperature distributions is inaccurate when temperature gradients are high, particularly in shock wave turbulent boundary layer interactions close to the wall. Complexities of fluid flow phenomena include transition to turbulence, relaminarization separated flows, transition between viscous and inviscid incompressible and compressible flows, among others, in all speed regimes. The purpose of this paper is to introduce a new approach, called the Flowfield-Dependent Mixed Explicit-Implicit (FDMEI) method, in an attempt to resolve these difficult issues in Computational Fluid Dynamics (CFD). In this process, a total of six implicitness parameters characteristic of the current flowfield are introduced. They are calculated from the current flowfield or changes of Mach numbers, Reynolds numbers, Peclet numbers, and Damkoehler numbers (if reacting) at each nodal point and time step. This implies that every nodal point or element is provided with different or unique numerical scheme according to their current flowfield situations, whether compressible, incompressible, viscous, inviscid, laminar, turbulent, reacting, or nonreacting. In this procedure, discontinuities or fluctuations of an variables between adjacent nodal points are determined accurately. If these implicitness parameters are fixed to certain numbers instead of being calculated from the flowfield information, then practically all currently available schemes of finite differences or finite elements arise as special cases. Some benchmark problems to be presented in this paper will show the validity, accuracy, and efficiency of the proposed methodology.
Document ID
19970023531
Acquisition Source
Langley Research Center
Document Type
Contractor Report (CR)
Authors
Garcia, S. M.
(Alabama Univ. Huntsville, AL United States)
Chung, T. J.
(Alabama Univ. Huntsville, AL United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1997
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NAS 1.26:205035
UAH-5-30226
NASA-CR-205035
Report Number: NAS 1.26:205035
Report Number: UAH-5-30226
Report Number: NASA-CR-205035
Accession Number
97N23849
Funding Number(s)
CONTRACT_GRANT: NGT1-52114
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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