Higher order staggered coupling schemes to predict the aeroelastic behavior of helicopter rotors

被引：0

作者：

Wagner, SN ^{[1
]}

Altmikus, A ^{[1
]}

机构：

[1] Univ Stuttgart, Inst Aerodynam & Gas Dynam, D-70550 Stuttgart, Germany

来源：

COMPUTATIONAL FLUID AND SOLID MECHANICS 2003, VOLS 1 AND 2, PROCEEDINGS | 2003年

关键词：

helicopter aeromechanics; fluid-structure coupling; aeroelasticity; staggered coupling schemes;

D O I：

暂无

中图分类号：

O3 [力学];

学科分类号：

08 ; 0801 ;

摘要：

Higher order staggered coupling schemes are presented to couple the calculation of the aerodynamics and structural dynamics of helicopter rotor blades in a modular manner. The continuous interference effects are replaced by discrete influence terms that are exchanged at synchronized instants. Comparisons of calculated loads of the blades with test results demonstrate the capability of the procedure.

引用

页码：1556 / 1559

页数：4

共 11 条

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[10] The effect of non-local higher order stress to predict the nonlinear vibration behavior of carbon nanotube conveying viscous nanoflow
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