The suitability of applying the overlapping grid method to parallel computation of steady and unsteady compressible inviscid flows with three-point block-tridiagonal implicit schemes is addressed in this paper. An easily usable interface treatment is constructed and analyzed for both steady and unsteady problems. The performance of the method, such as convergence rate and time accuracy, can be controlled through the overlapping width. The method needs no iteration at each time step or modification of the Thomas algorithm for the solution of the implicit parts. In both steady and unsteady cases a very good absolute parallel efficiency is demonstrated for bidimensional subsonic and transonic flow computations. (C) 2000 Academic Press.
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Univ Michigan, Dept Math, Ann Arbor, MI 48109 USAUniv Michigan, Dept Math, Ann Arbor, MI 48109 USA
Zaitzeff, Alexander
Esedoglu, Selim
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Univ Michigan, Dept Math, Ann Arbor, MI 48109 USAUniv Michigan, Dept Math, Ann Arbor, MI 48109 USA
Esedoglu, Selim
Garikipati, Krishna
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Univ Michigan, Michigan Inst Computat Discovery & Engn, Dept Mech Engn, Ann Arbor, MI 48109 USA
Univ Michigan, Michigan Inst Computat Discovery & Engn, Dept Math, Ann Arbor, MI 48109 USAUniv Michigan, Dept Math, Ann Arbor, MI 48109 USA
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China Univ Petr, State Key Lab Petr Resource & Prospecting, Beijing 102249, Peoples R China
Univ Texas Austin, Inst Geophys, John A & Katherine G Jackson Sch Geosci, Austin, TX 78758 USAChina Univ Petr, State Key Lab Petr Resource & Prospecting, Beijing 102249, Peoples R China
Liu, Yang
Sen, Mrinal K.
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Univ Texas Austin, Inst Geophys, John A & Katherine G Jackson Sch Geosci, Austin, TX 78758 USAChina Univ Petr, State Key Lab Petr Resource & Prospecting, Beijing 102249, Peoples R China