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Volumn 10, Issue 7, 2006, Pages 581-589

Application of multi-objective optimization to axial compressor preliminary design{star, open}{star, open}This article was presented at the German Aerospace Congress 2005.

Author keywords

Aerodynamic design; Axial compressor; Meanline prediction; Multi objective optimization

Indexed keywords

AERODYNAMIC DESIGN; AXIAL COMPRESSORS; MEANLINE PREDICTION; MULTI-OBJECTIVE OPTIMIZATION;

EID: 33749530201     PISSN: 12709638     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.ast.2006.03.007     Document Type: Article
Times cited : (43)

References (11)
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    • Engenious Software Inc., Process Integration and Optimization using iSight, http://www.engineous.com
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    • 33749529388 scopus 로고    scopus 로고
    • H. Klinger, Das Engine 3E Kerntriebwerk von Rolls-Royce Deutschland, DGLR Jahrestagung 2004, 2004-178, January 2004
  • 8
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    • Stalling pressure rise capability of axial flow compressor stages
    • Koch C.C. Stalling pressure rise capability of axial flow compressor stages. ASME JEP 103 (October 1981)
    • (1981) ASME JEP , vol.103
    • Koch, C.C.1
  • 10
    • 34250129599 scopus 로고
    • NLPQL: A Fortran subroutine solving constrained nonlinear programming problems
    • Schittkowski K. NLPQL: A Fortran subroutine solving constrained nonlinear programming problems. Annals of Operations Research 5 (1986) 485-500
    • (1986) Annals of Operations Research , vol.5 , pp. 485-500
    • Schittkowski, K.1
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    • 33749525329 scopus 로고    scopus 로고
    • 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


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.