Aerodynamic optimization design for airfoil based on Kriging model

Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica

Volumn 26, Issue 5, 2005, Pages 545-549

  Wang, Xiao Feng ^a   Xi, Guang ^a  

^a XI'AN JIAOTONG UNIVERSITY   (China)

Author keywords

Aerodynamics; Design of experiments; Kriging model; Optimization design

Indexed keywords

AERODYNAMICS; APPLICATIONS; APPROXIMATION THEORY; DRAG; GENETIC ALGORITHMS; GEOMETRY; LIFT; MATHEMATICAL MODELS; OPTIMIZATION; STRUCTURAL DESIGN;

KRIGING MODEL; LIFT DRAG RATIO; MACH NUMBER; OPTIMIZATION DESIGN;

AIRFOILS;

EID: 33645650947     PISSN: 10006893     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (6)

1. Schmit L A, Farshi B. Some approximation concepts for structural synthesis[J]. AIAA J, 1974, 12(5): 692-699.
2. Sacks J, Welch W J, Mitchell T J, et al. Design and analysis of computer experiments[J]. Statistical Science, 1989, 4(4): 409-435.
3. Montgomery D C. Design and analysis of experiments[M]. New York: John Wiley and Sons, 1997.
4. Fang K T. Uniform design and uniform design table[M]. Beijing: Science Press, 1994. (in Chinese)
5. Zhu Z Q, Fu H Y, Xu R X, et al. Multiobjective optimization design research of the aerofoil and wing[J]. Science China (Series E), 2003, 33(11): 999-1006. (in Chinese)
6. FINE/TURBO. Manual: NUMECA'S flow integrated environment for turbomachaery and internal flows[M]. User manual Version 6.1. Brussels, 2003.