SOLUTION OF 2-D TRANSONIC CASCADE FLOW WITH EFFECTIVE FLUX VECTOR-SPLITTING IMPLICIT SCHEME

Jan. 1994

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Article Navigation > Journal of Aerospace Power > 1994 > 9(1): 79-82

SOLUTION OF 2-D TRANSONIC CASCADE FLOW WITH EFFECTIVE FLUX VECTOR-SPLITTING IMPLICIT SCHEME[J]. Journal of Aerospace Power, 1994, 9(1): 79-82.

Citation:

SOLUTION OF 2-D TRANSONIC CASCADE FLOW WITH EFFECTIVE FLUX VECTOR-SPLITTING IMPLICIT SCHEME[J]. Journal of Aerospace Power, 1994, 9(1): 79-82.

SOLUTION OF 2-D TRANSONIC CASCADE FLOW WITH EFFECTIVE FLUX VECTOR-SPLITTING IMPLICIT SCHEME[J]. Journal of Aerospace Power, 1994, 9(1): 79-82.

Citation:

SOLUTION OF 2-D TRANSONIC CASCADE FLOW WITH EFFECTIVE FLUX VECTOR-SPLITTING IMPLICIT SCHEME[J]. Journal of Aerospace Power, 1994, 9(1): 79-82.

Abstract

Abstract A one step effective flux vector splitting implicit scheme is developed,which features simplicity of no approximate factorization and no block bidiagonal system of equations.The scheme provides a significant enhancement in computational efficiency because it has advantageous characteristics in creation of higher order numerical implicit items.The Euler flow of a two dimensional cascade is calculated numerically by using the above scheme,and the results show that it has good convergence and accuracy of shock wave capture.