메뉴 건너뛰기




Volumn 5 B, Issue , 2004, Pages 1481-1490

Application of multipoint optimization to the design of turbomachinery blades

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL COMPLEXITY; COMPUTER AIDED DESIGN; DATABASE SYSTEMS; GENETIC ALGORITHMS; NEURAL NETWORKS; ROTORS; SIMULATED ANNEALING;

EID: 10244222290     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/gt2004-53110     Document Type: Conference Paper
Times cited : (64)

References (8)
  • 5
    • 10244271111 scopus 로고    scopus 로고
    • Effect of flow rate on the development of three-dimensional flow in NASA LSCC impeller, based on numerical solutions
    • S. Kang, Ch. Hirsch, 1999, "Effect of flow rate on the development of three-dimensional flow in NASA LSCC impeller, based on numerical solutions, ISABE Paper No. 99-7225.
    • (1999) ISABE Paper No. 99-7225 , vol.99 , Issue.7225
    • Kang, S.1    Hirsch, Ch.2
  • 7
    • 84894383101 scopus 로고    scopus 로고
    • Designing turbomachinery blades with the function approximation concept and the Navier-Stokes equations
    • Long Beach, CA
    • Pierret, S., Demeulenaere, A., Gouverneur, B., Hirsch, C., "Designing Turbomachinery Blades with the Function Approximation Concept and the Navier-Stokes Equations", 8th AIAA/NASA/USAF/ISSMO Symposium on MDO, Long Beach, CA (2000).
    • (2000) 8th AIAA/NASA/USAF/ISSMO Symposium on MDO
    • Pierret, S.1    Demeulenaere, A.2    Gouverneur, B.3    Hirsch, C.4


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.