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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1986, Vol. 7 ›› Issue (5): 490-493.
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Zhang Lumin, Shan Xiaonan
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The split-coefficient matrix (SCM) for solving inviscid flow over the asymmetric nose-cone is presented. According to SCM technique, governing equations are solved by MacCormack's second-order scheme in a predictor-corrector sequence. The present paper presents the numerical results of the flow field and aerodynamic characteristics over an asymmetric nose-cone.The accuracy analyses of the results are also given in this paper.
Zhang Lumin;Shan Xiaonan. SPLIT-COEFFICIENT MATRIX FINIT DIFFERENCE METHOD FOR THE ASYMMETRIC NOSE-CONE[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1986, 7(5): 490-493.
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https://hkxb.buaa.edu.cn/EN/Y1986/V7/I5/490