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从翼剖面理论分析着手对亚、超音速非线性平衡转速进行了机理探讨,对十字斜切翼-弹身-涡轮组合体给出了较实用而可靠的转速计算方法,并与实验值作了比较。本文可供火箭弹(丸)设计、外弹道计算以及风洞旋转试验参考。
Based on the theoretical analysis of wing profile, the mechanism of sub-supersonic and non-linear equilibrium rotational speed is discussed. The practical and reliable calculation method of rotational speed is given for the cross-beveled wing-body-turbine combination. The experimental results are compared with the experimental data Compare This article is available for rockets (pills) design, calculation of external ballistics and wind tunnel rotation test reference.