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复合材料旋翼桨叶剖面扭转刚度计算
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(2).
作者姓名:许钟  邹振民  樊蔚勋
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。

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
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(2).
Authors:Xu Zhong Zou Zhenmin Fan Weixun
Institution:Xu Zhong Zou Zhenmin Fan Weixun
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.
Keywords:composite materials  rotor blades  torsional rigidity    
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