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本文根据缩比为1/10和1/13的S导弹模型分别在0.6m~2风洞所进行的全弹零升前阻与底阻的实验结果,并综合了在该风洞中进行的喷流、通气以及雷诺数效应等专项实验研究结果。阐述了零升总阻的修正体系。由其而预计的S导弹全尺寸零升总阻与飞行测量值有着很好的一致性。其研究方法可供其它导弹参考。
Based on the experimental results of the full-bomb zero-rise front drag and the bottom drag conducted by the S missile model with 1/10 scale and 1/13 scale respectively in 0.6m ~ 2 wind tunnels, Jet, ventilation and Reynolds number effects and other special experimental results. The zero-liter total resistance correction system is described. It is estimated that the full-size zero-lift S-missile total resistance and flight measurements have a good consistency. Its research method is available for other missiles.