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本文虽属对驾束制导导弹的研究,但对旋转弹翼式的气动外形的特性分析较多,因此,对搞总体工作的同志可能有些参考价值。
Although this article is a study of the beam-guided missile, the characteristics of the aerodynamic shape of the rotor-propelled wing are more analyzed. Therefore, there may be some reference values to the comrades engaged in the overall work.