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Volumn , Issue , 1999, Pages

A linear approach to the multi-parameter design of three-dimensional turbomachinery blades

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; ASPECT RATIO; DESIGN; DIFFERENTIATION (CALCULUS); HEURISTIC METHODS; KINETIC ENERGY; KINETICS; MACHINERY; NOZZLE DESIGN; PERTURBATION TECHNIQUES;

EID: 84983113742     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (6)

References (16)
  • 1
    • 0026932967 scopus 로고
    • Methodology for calculating Aerodynamic Sensitivity Derivatives
    • Taylor, A.C., Hou, G.W. and Korivi, V.M.; "Methodology for calculating Aerodynamic Sensitivity Derivatives", AIAA Journal, vol 30, no 10, pp2411-2419, 1992.
    • (1992) AIAA Journal , vol.30 , Issue.10 , pp. 2411-2419
    • Taylor, A.C.1    Hou, G.W.2    Korivi, V.M.3
  • 8
    • 0141699643 scopus 로고    scopus 로고
    • A Forward and Inverse Three-Dimensional Linear Design System for Turbomachinery Applications
    • Sept., Athens, Greece
    • Shahpar, S. and Lapworth, B.L.; "A Forward and Inverse Three-Dimensional Linear Design System for Turbomachinery Applications", 4th ECCOMAS Computational Fluid Dynamics Conference, Sept., 1998, Athens, Greece.
    • (1998) 4Th ECCOMAS Computational Fluid Dynamics Conference
    • Shahpar, S.1    Lapworth, B.L.2
  • 9
    • 20544476549 scopus 로고
    • Aerodynamic design via control theory
    • Jameson, A. "Aerodynamic design via control theory", J. Sci. Comput., vol 3, pp233-260, 1988.
    • (1988) J. Sci. Comput , vol.3 , pp. 233-260
    • Jameson, A.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.