然后应用中心复合试验设计法确定了七十种外形布局，并计算和分析了各外形参数变化对联结翼飞机稳定性的影响。
According to the computing results, the relations between the he stability characteristics and the configuration parameters of joined-wing airplanes were obtained.
初步的预分析结果表明，中心复合旋转设计方法可以满足本项目的精度要求，而且具有相当高的工作效率，所以该试验设计方法被采用。
Initial review study identified the central composite rotatable design (CCRD) method as an appropriate method for efficient experiment design within the context of response surface calibration.
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