The calculating results of this method for the C-5A aircraft wing are fairly close to that of implicit finite-difference method using Cebecis algebraic turbulent model.
对C - 5a机翼的计算结果表明，该方法具有同微分方法可以比拟的计算精度。
The calculating results of this method for the C-5A aircraft wing are fairly close to that of implicit finite-difference method using Cebecis algebraic turbulent model.
对C - 5a机翼的计算结果表明，该方法具有同微分方法可以比拟的计算精度。
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