| 复合材料旋翼桨叶剖面扭转刚度计算 |
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| 引用本文： | 许钟,邹振民,樊蔚勋. 复合材料旋翼桨叶剖面扭转刚度计算[J]. 南京航空航天大学学报, 1988, 0(2) |
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| 作者姓名： | 许钟 邹振民 樊蔚勋 |
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| 摘 要： | 本文对Krahula,J.L.等人提出的“圣维南扭转的有限元解”作了合理的改进,使改进后的公式能很方便地编成计算程序,作复合材料旋翼桨叶的扭转刚度计算。还应用改进后的公式计算了两种型号直升机旅翼桨叶的扭转刚度,计算值和试验值有很好的一致性。
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| 关 键 词： | 复合材料 旋翼桨叶 扭转刚度 |
Calculation of the Torsional Stiffness at a Cross Setcion of a Composite Rotor Blade |
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| Xu Zhong Zou Zhenmin Fan Weixun. Calculation of the Torsional Stiffness at a Cross Setcion of a Composite Rotor Blade[J]. Journal of Nanjing University of Aeronautics & Astronautics, 1988, 0(2) |
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| Authors: | Xu Zhong Zou Zhenmin Fan Weixun |
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| Affiliation: | Xu Zhong Zou Zhenmin Fan Weixun |
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| Abstract: | The finite element solution for Saint-Venant Torsion presented by Krahula, J.L. and Lauterbach, G.F. is reasonably improved in this paper, and it is quite convenient to compile a computer program with the improved formula. The numerical results of calculating the torsional stiffness of a rotor blade cross section of two types of helicopters are thus obtained from the improved formula, and the calculating results are compared with their experimental values in good agreement. |
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| Keywords: | composite materials rotor blades torsional rigidity. |
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