Multi-objective optimization of three-dimensional blade shape for an axial compressor rotor in transonic stage

被引：0

作者：

Myoren, Chihiro ^{[1
]}

Takahashi, Yasuo ^{[1
]}

Kato, Yasuhiro ^{[1
]}

机构：

[1] Hitachi Laboratory, Hitachi, Ltd., 7-1-1 Omika-cho, Hitachi-shi, 319-1221, Japan

来源：

International Journal of Gas Turbine, Propulsion and Power Systems | 2013年 / 5卷 / 01期

关键词：

D O I：

暂无

中图分类号：

学科分类号：

摘要：

引用

页码：8 / 16

共 50 条

[1] Three-dimensional multi-objective design optimization of a transonic compressor rotor
Benini, E
JOURNAL OF PROPULSION AND POWER, 2004, 20 (03) : 559 - 565
[2] Multi-objective optimization of an axial compressor blade
Abdus Samad
Kwang-Yong Kim
Journal of Mechanical Science and Technology, 2008, 22 : 999 - 1007
[3] Multi-objective optimization of an axial compressor blade
Samad, Abdus
Kim, Kwang-Yong
JOURNAL OF MECHANICAL SCIENCE AND TECHNOLOGY, 2008, 22 (05) : 999 - 1007
[4] Shape optimization of an axial compressor blade by multi-objective genetic algorithm
Samad, A.
Kim, K-Y
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY, 2008, 222 (A6) : 599 - 611
[5] Three-dimensional optimization of squealer-tip for a transonic axial-flow compressor rotor blade
Shahri, Mojtaba Heidarian
Habibzadeh, Saeid
Madadi, Ali
HELIYON, 2024, 10 (01)
[6] Optimization Of Rotor Blade In Stage Circumstance For Transonic Axial Flow Compressor
Cheng, Jinxin
Chen, Jiang
Xiang, Hang
PROCEEDINGS OF THE 2017 12TH IEEE CONFERENCE ON INDUSTRIAL ELECTRONICS AND APPLICATIONS (ICIEA), 2017, : 1774 - 1779
[7] MULTI-OBJECTIVE CONSTRAINED AERO-MECHANICAL OPTIMIZATION OF AN AXIAL COMPRESSOR TRANSONIC BLADE
Astrua, Pio
Piola, Stefano
Silingardi, Andrea
Bonzani, Federico
PROCEEDINGS OF THE ASME TURBO EXPO 2012, VOL 8, PTS A-C, 2012, : 241 - 252
[8] Optimization of blade sweep in a transonic axial compressor rotor
Jang, CM
Li, P
Kim, KY
JSME INTERNATIONAL JOURNAL SERIES B-FLUIDS AND THERMAL ENGINEERING, 2005, 48 (04) : 793 - 801
[9] Sweep optimization on a transonic rotor blade of an axial compressor
National Key Lab. on Aero-Engine, School of Jet Propulsion, Beihang University, Beijing 100083, China
Kung Cheng Je Wu Li Hsueh Pao, 2007, SUPPL. 1 (109-112):
[10] Multi-objective optimization of transonic compressor blade using evolutionary algorithm
Lian, YS
Liou, MS
JOURNAL OF PROPULSION AND POWER, 2005, 21 (06) : 979 - 987

← 1 2 3 4 5 →