DEVELOPMENT OF A HIGHER-ORDER ACCURATE RECONSTRUCTION SCHEME WITH REDUCED LEAST SQUARE MATRIX FOR CONVECTIVE AND DIFFUSIVE FLUX EVALUATION

被引:1
作者
Nair, Praveen [1 ]
Jayachandran, T. [1 ]
Puranik, Bhal Chandra [2 ]
Bhandarkar, V. Upendra [2 ]
机构
[1] Vikram Sarabhai Space Ctr, Indian Space Res Org, Prop Grp, Trivandrum 695022, Kerala, India
[2] Indian Inst Technol, Dept Mech Engn, Bombay 400076, Maharashtra, India
关键词
Reduced least square matrix; unstructured meshes; higher-order reconstruction; solution mapped; high altitude test facility; high-speed flows; HYPERSONIC FLOWS; COMPUTATIONS; SEQUEL; AUSM;
D O I
10.1142/S0219876209001929
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
The development of a higher-order reconstruction scheme with reduced least square matrix is presented. The matrix used in conventional least square based reconstruction schemes for finite volume solvers contains bigger terms. For solution dependent schemes, this matrix has to be inverted for each time step, which is computationally costlier. To overcome this, certain mathematical principles applicable to finite volume formulation, have been used to eliminate a good number of terms appearing in the matrix. In addition, accurate and computationally efficient derivative plug-ins are incorporated to make the formulation generalized so that one can extend it to any order of accuracy. The presence of higher derivative terms in this scheme ensures uniformly higher-order accuracy throughout the flow domain. The reduced matrix can be used for data independent as well as solution dependent reconstruction schemes. Computationally efficient stencil searching algorithm, satisfying physical and topological requirements and capable of handling structured, unstructured, and adaptive grids has been coupled with the scheme. The scheme has been successfully used to simulate flow over blunt cone-flare, NASA B2 nozzle, and high altitude test facility. The solver has shown around 30% saving in least square matrix evaluation time.
引用
收藏
页码:425 / 446
页数:22
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