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Volumn , Issue , 2003, Pages 11-21

Summary of the Delft University wind turbine dedicated airfoils

Author keywords

[No Author keywords available]

Indexed keywords

AIRFOILS; ANGLE OF ATTACK; DESIGN FOR TESTABILITY; LIFT; WIND POWER; WIND TUNNELS; WIND TURBINES;

EID: 70349100672     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/wind2003-352     Document Type: Conference Paper
Times cited : (27)

References (14)
  • 4
    • 78049454575 scopus 로고    scopus 로고
    • The performance of new wind turbine blade tip and root airfoils up to high angles-of-attack
    • W.A. Timmer, R. van Rooij, "The performance of new wind turbine blade tip and root airfoils up to high angles-of-attack". EWEC 1997, Dublin, Ireland
    • EWEC 1997, Dublin, Ireland
    • Timmer, W.A.1    Van Rooij, R.2
  • 5
    • 0347901092 scopus 로고    scopus 로고
    • Measured section performance of rotating blades as input to the design of inboard airfoils
    • W.A. Timmer, R. van Rooij, "measured section performance of rotating blades as input to the design of inboard airfoils". EWEC 1999, Nice, France
    • EWEC 1999, Nice, France
    • Timmer, W.A.1    Van Rooij, R.2
  • 6
    • 77953795074 scopus 로고    scopus 로고
    • Some aspects of high angle-of-attack flow on airfoils for wind turbine application
    • W.A. Timmer, R. van Rooij, "Some aspects of high angle-of-attack flow on airfoils for wind turbine application". EWEC 2001, Copenhagen, Denmark
    • EWEC 2001, Copenhagen, Denmark
    • Timmer, W.A.1    Van Rooij, R.2
  • 7
    • 0003913801 scopus 로고
    • Wall interference in a two-dimensional wind tunnel, with consideration of the effect of compressibility
    • H.J. Allen, W.G. Vincenti, "Wall interference in a two-dimensional wind tunnel, with consideration of the effect of compressibility." NACA Report no. 782, 1947.
    • (1947) NACA Report No. 782
    • Allen, H.J.1    Vincenti, W.G.2
  • 8
    • 0003209770 scopus 로고
    • Simplified method for the determination of critical height of distributed roughness particles for boundary-layer transition at Mach numbers from 0 to 5
    • A.L. Braslow, E.C. Knox, "Simplified method for the determination of critical height of distributed roughness particles for boundary-layer transition at Mach numbers from 0 to 5". NACA Technical Note 4363, 1958
    • (1958) NACA Technical Note 4363
    • Braslow, A.L.1    Knox, E.C.2
  • 14
    • 33747342401 scopus 로고
    • A correlation of low-speed airfoil-section stalling characteristics with Reynolds number and airfoil geometry
    • Washington, March
    • D.E. Gault, A correlation of low-speed airfoil-section stalling characteristics with Reynolds number and airfoil geometry. NACA Technical Note 3963, Washington, March 1957
    • (1957) NACA Technical Note 3963
    • Gault, D.E.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.