| Citation: | JIN Dong-hai, GUI Xing-min. Numerical design optimization of compressor blade based on ADOP[J]. Journal of Aerospace Power, 2007, 22(11): 1903-1908. |
| [1] |
Gardner B A,Selig M S.Airfoil design using a genetical gorit hm and an inver se meth od[R].A IA A 2003 0043.
|
| [2] |
Mengist u T,Ghaly W.Singl e and mult i point shape optimiz at ion of gas tu rbine bl ade cascades[R].A IA A 20044446.
|
| [3] |
ZHU Ziqiang,FU Hongyan,YU Rixin et al.M ult i ob jec t ive design opt im izat ion of airf oil an d w ing[J].Science in Ch ina,2003,33(11):999 1006.
|
| [4] |
Obayash i S,Tsu kahara T,N akamura T.Multiobjective genet ic algorit hm applied t o aerodynamic des ign of cascade airf oils[J].IE EE Tran sact ions on Indu st rial Elect ronics,2000,47(1):211 216.
|
| [5] |
FANG Kait ai.Unif orm d esign and un iform des ign t able[M].Bei jing:S cien ce Pres s,1994.
|
| [6] |
Terry L.A erodynam ic shape opt imizat ion using a real number encoded genet ic al gorit hm[R].A IA A 2001 2473.
|
| [7] |
JIN Don ghai,GUI Xin gmin.A erodyn amic design opt imization of cascade airf oil based on mult iobject ive gen et ic algorit hm[J].Journal of Aerospace Pow er,2007,22(2):285 290.
|
| [8] |
JIN Donghai,CH EN Jia,G U I Xingmin.Mult i poi nt aer odynamic design opt imiz at ion for compressor cascade air f oils[J].Journal of Propu lsion T ech nology,2007,28(4):367 372.
|
| [9] |
Rai M M.Tow ards a hybrid aerodyn ami c des ign procedure based on neural net work s and evol ut ionary met h ods[R].A IA A 2002 3143.
|
| [10] |
CHEN Kui.Design of experiment and analysis[M].Beijing:T singhu a U niversit y Pr ess,2005.
|