EXPERIMENTS AND ANALYSIS FOR COMPOSITE BLADES UNDER LARGE DEFLECTIONS .1. STATIC BEHAVIOR

被引：65

作者：

MINGUET, P

DUGUNDJI, J

机构：

[1] Technology Laboratory for Advanced Composites, Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, Cambridge, MA

[2] Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, Cambridge, MA

来源：

AIAA JOURNAL | 1990年 / 28卷 / 09期

关键词：

Aircraft Materials--Composite Materials - Epoxy Resins--Fiber Reinforcement - Mathematical Techniques--Finite Difference Method - Plastics; Reinforced--Graphite Fiber - Structural Analysis;

D O I：

10.2514/3.25255

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

The static behavior of structurally coupled composite blades is investigated analytically and experimentally in this paper. A model, based on the use of Euler angles, is developed that can account for the presence of arbitrarily large deflections without the need for any ordering scheme. A simple iterative finite-difference solution procedure is then presented. Some experiments using thin flat composite cantilevered beams are also performed, and the data obtained compare well with the results from the analysis. © 1990 American Institute of Aeronautics and Astronautics, Inc., All rights reserved.

引用

页码：1573 / 1579

页数：7