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Volumn 39, Issue 6, 2001, Pages 1047-1056

Sensitivity analysis of unsteady inviscid flow through turbomachinery cascades

Author keywords

[No Author keywords available]

Indexed keywords

ACCELERATION; AERODYNAMIC LOADS; AERODYNAMICS; AIRFOILS; CASCADES (FLUID MECHANICS); COMPUTATIONAL FLUID DYNAMICS; DIFFERENTIAL EQUATIONS; MATHEMATICAL MODELS; SENSITIVITY ANALYSIS; STEADY FLOW; UNSTEADY FLOW;

EID: 0035369602     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.1445     Document Type: Article
Times cited : (28)

References (24)
  • 17
    • 0004081558 scopus 로고
    • A numerical analysis of 3-D inviscid stator/rotor interactions using non-reflecting boundary conditions
    • Massachusetts Inst. of Technology, Cambridge, MA, March
    • (1992) Gas Turbine Lab. Rept. 209
    • Saxer, A.P.1
  • 19
    • 0020209106 scopus 로고
    • A multiple grid scheme for solving the Euler equations
    • (1982) AIAA Journal , vol.20 , Issue.11 , pp. 1565-1571
    • Ni, R.1
  • 21
    • 4243706964 scopus 로고
    • Force and moment for vibratory aerofoils in cascades
    • British Aeronautical Research Council, R and M 3254, London
    • (1960)
    • Whitehead, D.S.1
  • 24
    • 0003392825 scopus 로고
    • Aeroelasticity in turbomachines. Comparison of theoretical and experimental results
    • U.S. Air Force Office of Scientific Research, AFOSR-TR-87-0605, Washington, DC
    • (1986)
    • Bölcs, A.1    Fransson, T.H.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.