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Volumn 6 PART B, Issue , 2006, Pages 1209-1216

Modern compressor aerodynamic blading process using multi-objective optimization

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC BLADING PROCESS; AERODYNAMIC DESIGNS; MULTI OBJECTIVE OPTIMIZATION; RADIAL STACKING LINES; ROLLS ROYCE (CO);

EID: 33750845634     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/GT2006-90206     Document Type: Conference Paper
Times cited : (12)

References (12)
  • 1
    • 33750852599 scopus 로고    scopus 로고
    • Application of multi-objective optimization to axial compressor preliminary design
    • A. Keskin and D. Bestle. Application of Multi-Objective Optimization to Axial Compressor Preliminary Design. DGLR Jahrestagung, DGLR-2005-192, 2005.
    • (2005) DGLR Jahrestagung, DGLR-2005-192
    • Keskin, A.1    Bestle, D.2
  • 2
    • 0008065596 scopus 로고
    • A general theory of three-dimensional flow in subsonic and supersonic turbomachines of axial, radial, and mixed-flow types
    • C.-H. Wu. A General Theory of Three-Dimensional Flow in Subsonic and Supersonic Turbomachines of Axial, Radial, and Mixed-Flow Types. NACA TN 2604, 1952.
    • (1952) NACA TN , vol.2604
    • Wu, C.-H.1
  • 3
    • 0033052812 scopus 로고    scopus 로고
    • Automatic genetic optimization approach to two-dimensional blade profile design for steam turbines
    • M. A. Trigg, G. R. Tubby, and A. G. Shreard. Automatic Genetic Optimization Approach to Two-Dimensional Blade Profile Design for Steam Turbines. Journal of Turbomachinery, ASME, Vol. 121:11-17, 1999.
    • (1999) Journal of Turbomachinery, ASME , vol.121 , pp. 11-17
    • Trigg, M.A.1    Tubby, G.R.2    Shreard, A.G.3
  • 4
    • 0034233213 scopus 로고    scopus 로고
    • Development of advanced compressor airfoils for heavy-duty gas turbines - Part I: Design and opimization
    • U. Koeller, R. Moenig, B. Kuesters, and H.-A. Schreiber. Development of Advanced Compressor Airfoils for Heavy-Duty Gas Turbines - Part I: Design and Opimization. Journal of Turbomachinery, ASME, Vol. 122:397-405, 2000.
    • (2000) Journal of Turbomachinery, ASME , vol.122 , pp. 397-405
    • Koeller, U.1    Moenig, R.2    Kuesters, B.3    Schreiber, H.-A.4
  • 5
    • 7644238600 scopus 로고    scopus 로고
    • Design of industrial axial compressor blade sections for optimal range and performance
    • F. Sieverding, B. Ribi, M. Casey, and M. Meyer. Design of Industrial Axial Compressor Blade Sections for Optimal Range and Performance. Journal of Turbomachinery ASME, Vol. 126:323-331, 2004.
    • (2004) Journal of Turbomachinery ASME , vol.126 , pp. 323-331
    • Sieverding, F.1    Ribi, B.2    Casey, M.3    Meyer, M.4
  • 11
    • 0019070772 scopus 로고
    • Natural transition of boundary layers - The effects of turbulence, pressure gradient, and flow history
    • B. J. Abu-Ghannam and R. Shaw. Natural transition of boundary layers - The effects of turbulence, pressure gradient, and flow history. Journal of Mechanical Engineering Science, 22(5):213-228, 1980.
    • (1980) Journal of Mechanical Engineering Science , vol.22 , Issue.5 , pp. 213-228
    • Abu-Ghannam, B.J.1    Shaw, R.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.