TY - GEN
T1 - Determination of linear and nonlinear parameters of combustion chamber wall materials
AU - Riccius, Jörg R.
AU - Haidn, Oskar J.
PY - 2003
Y1 - 2003
N2 - A study for the determination of elastic and elastoplastic parameters of a typical combustion chamber material (Cu alloy) with different test sample geometries is presented. Based on the experimental results of elastic and elasto-plastic tests of three sample geometries the appropriate elasto-plastic parameters such as yield stress and hardening parameters are determined. Furthermore, details about the loading during the tests, the advantages and disadvantages of each of the sample geometries and of the appropriate range of testing are pointed out. Cyclic fatigue calculations using FEM which assumes either kinematic hardening or isotropic hardening showed that neither of the methods alone was able to reproduce the experimentally determined material behavior. Finally, by the use of a combination of nonlinear kinematic and multi linear isotropic hardening, a satisfying agreement between experiment and FEM predictions could be obtained.
AB - A study for the determination of elastic and elastoplastic parameters of a typical combustion chamber material (Cu alloy) with different test sample geometries is presented. Based on the experimental results of elastic and elasto-plastic tests of three sample geometries the appropriate elasto-plastic parameters such as yield stress and hardening parameters are determined. Furthermore, details about the loading during the tests, the advantages and disadvantages of each of the sample geometries and of the appropriate range of testing are pointed out. Cyclic fatigue calculations using FEM which assumes either kinematic hardening or isotropic hardening showed that neither of the methods alone was able to reproduce the experimentally determined material behavior. Finally, by the use of a combination of nonlinear kinematic and multi linear isotropic hardening, a satisfying agreement between experiment and FEM predictions could be obtained.
UR - http://www.scopus.com/inward/record.url?scp=84897586236&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:84897586236
SN - 9781624100987
T3 - 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
BT - 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
T2 - 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2003
Y2 - 20 July 2003 through 23 July 2003
ER -