Numerical analysis calculates transonic flow around a circular airfoil, suggesting effectiveness of hybrid schemes.
A mixed difference scheme called hybrid scheme, which is initiated in Reference 1 and is shown to be effective particularly for computation of transonic flow, is applied to calculate the transonic flow around a circular airfoil. The result is compared with those obtained by the MacCormack scheme and the hybrid one in Reference 1.
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Wang et al. (1984) studied this question.
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