TY - JOUR
T1 - Multidisciplinary optimization design system for turbine blade
AU - Wang, Jing Chao
AU - Li, Li Zhou
AU - Yue, Zhu Feng
PY - 2007/1
Y1 - 2007/1
N2 - An integrated, three-dimensional, multi-disciplinary optimization design system for turbine blades has been set up, which enables the design and analysis of certain blades optimized involving five disciplines. In this system, quintic polynomial is used for parameter modeling of three-dimensional turbine blades, and unit linear interpolation method used for transfer of interdisciplinary load information, while MIGA (Multi-island Genetic Algorithm) and SQP (Sequential Quadratic Programming) are used for overall optimization. The case study shows that, optimization efforts could improve greatly the performance of turbine blades, and the system exhibits higher stability, feasibility and efficiency for engineering applications.
AB - An integrated, three-dimensional, multi-disciplinary optimization design system for turbine blades has been set up, which enables the design and analysis of certain blades optimized involving five disciplines. In this system, quintic polynomial is used for parameter modeling of three-dimensional turbine blades, and unit linear interpolation method used for transfer of interdisciplinary load information, while MIGA (Multi-island Genetic Algorithm) and SQP (Sequential Quadratic Programming) are used for overall optimization. The case study shows that, optimization efforts could improve greatly the performance of turbine blades, and the system exhibits higher stability, feasibility and efficiency for engineering applications.
KW - Aerospace propulsion system
KW - All-at-once (AAO)
KW - Elemental linear interpolation (ELI)
KW - Multidisciplinary design optimization (MDO)
KW - Turbine blade
UR - http://www.scopus.com/inward/record.url?scp=33847790650&partnerID=8YFLogxK
M3 - 文章
AN - SCOPUS:33847790650
SN - 1000-8055
VL - 22
SP - 23
EP - 29
JO - Hangkong Dongli Xuebao/Journal of Aerospace Power
JF - Hangkong Dongli Xuebao/Journal of Aerospace Power
IS - 1
ER -