Comparison of residual strains measured by X-ray and neutron diffraction in a titanium (Ti-6Al-4V) matrix composite

被引:56
作者
Rangaswamy, P
Prime, MB
Daymond, M
Bourke, MAM
Clausen, B
Choo, H
Jayaraman, N
机构
[1] Univ Calif Los Alamos Natl Lab, Manuel Lujan Jr Neutron Scattering Ctr, Los Alamos, NM 87545 USA
[2] Rutherford Appleton Lab, ISIS, Didcot OX11 0QX, Oxon, England
[3] Univ Cincinnati, Dept Mat Sci & Engn, Cincinnati, OH 45221 USA
来源
MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING | 1999年 / 259卷 / 02期
关键词
residual stress; neutron diffraction; titanium matrix composites; finite element analysis; X-ray measurement;
D O I
10.1016/S0921-5093(98)00893-4
中图分类号
TB3 [工程材料学];
学科分类号
0805 ; 080502 ;
摘要
This research compares matrix thermal residual strains measured in a continuous fiber reinforced SiC/Ti-6Al-4V titanium matrix composite (TMC) using X-ray and neutron diffraction with finite element predictions. The strain dependence on the strains for several reflections (105, 204, 300, 213 and 312) of the matrix were explored at the surface (X-ray) and in the bulk (neutron). To determine the longitudinal surface strains from the X-ray measurements for comparison with the neutron values, the E-phi psi versus sin(2)psi plots were extrapolated to psi = 90 degrees. Continuum micro-mechanics based multi-ply finite element models (FEM) simulating rectangular and hexagonal fiber distributions were explored for calculating average surface and bulk strains. For different reflections, the experimentally determined surface measured strains ranged from + 1904 + 424 to + 2974 +/- 321 mu epsilon and the bulk measurements ranged from + 2269 +/- 421 to +/- 3022 +/- 1134 mu epsilon. These values contrast with the single valued FEM prediction of + 3200 mu epsilon which was the same for both the surface and the bulk. (C) 1999 Elsevier Science S.A. All rights reserved.
引用
收藏
页码:209 / 219
页数:11
相关论文
共 23 条
[1]  
BIGELOW CA, 1989, MECH COMPOSITE MAT S, P21
[2]  
CLAUSEN B, 1998, IN PRESS ACTA METT
[3]   DETERMINATION OF RESIDUAL-STRESSES IN THIN SHEET TITANIUM ALUMINIDE COMPOSITES [J].
COX, BN ;
JAMES, MR ;
MARSHALL, DB ;
ADDISON, RC .
METALLURGICAL TRANSACTIONS A-PHYSICAL METALLURGY AND MATERIALS SCIENCE, 1990, 21 (10) :2701-2707
[4]  
Cullity BD, 1978, ELEMENTS XRAY DIFFRA
[5]  
GIGERNZER H, 1989, TITANIUM ALUMINIDE C, P251
[6]   THE STATE OF RESIDUAL-STRESS IN THE NEAR-SURFACE REGION OF HOMOGENEOUS AND HETEROGENEOUS MATERIALS AFTER GRINDING [J].
HAUK, VM ;
OUDELHOVEN, RWM ;
VAESSEN, GJH .
METALLURGICAL TRANSACTIONS A-PHYSICAL METALLURGY AND MATERIALS SCIENCE, 1982, 13 (07) :1239-1244
[7]  
JAMES MR, 1993, RESIDUAL STRESSES IN COMPOSITES, P177
[8]  
JAMES MR, 1992, RESIDUAL STRESSES - III : SCIENCE AND TECHNOLOGY, VOLS 1 AND 2, P555
[9]  
JAMES MR, 1989, INT C RES STRESS, V2, P429
[10]   THE CHARACTERIZATION OF AN SCS6/TI-6A1-4V MMC INTERPHASE [J].
JONES, C ;
KIELY, CJ ;
WANG, SS .
JOURNAL OF MATERIALS RESEARCH, 1989, 4 (02) :327-335