메뉴 건너뛰기




Volumn 128, Issue 4, 2006, Pages 422-431

Experimental analysis of thick blunt trailing-edge wind turbine airfoils

Author keywords

[No Author keywords available]

Indexed keywords

CHORD RATIO; FLATBACK AIRFOILS; PRESSURE SURFACES; THICK BLUNT TRAILING-EDGES;

EID: 33845572520     PISSN: 01996231     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.2346701     Document Type: Article
Times cited : (118)

References (31)
  • 1
    • 3142769129 scopus 로고    scopus 로고
    • Innovative design approaches for large wind turbine blades
    • Report No. SAND2003-0723
    • TPI Composites, 2003, "Innovative Design Approaches for Large Wind Turbine Blades," Report No. SAND2003-0723.
    • (2003) TPI Composites
  • 2
    • 3142769129 scopus 로고    scopus 로고
    • Innovative design approaches for large wind turbine blades - Final report
    • Report No. SAND2004-0074
    • TPI Composites, 2004, "Innovative Design Approaches for Large Wind Turbine Blades - Final Report," Report No. SAND2004-0074.
    • (2004) TPI Composites
  • 3
    • 0348252419 scopus 로고    scopus 로고
    • Aerodynamic analysis of blunt trailing edge airfoils
    • Standish, K. J., and van Dam, C. P., 2003, "Aerodynamic Analysis of Blunt Trailing Edge Airfoils," ASME J. Sol. Energy Eng., 125(4), pp. 479-487.
    • (2003) ASME J. Sol. Energy Eng. , vol.125 , Issue.4 , pp. 479-487
    • Standish, K.J.1    Van Dam, C.P.2
  • 4
    • 20544474054 scopus 로고    scopus 로고
    • Innovative design approaches for large wind turbine blades
    • Jackson, K., Zuteck, M., van Dam, C. P., Standish, K. J., and Berry, D., 2005, "Innovative Design Approaches for Large Wind Turbine Blades," Wind Energy, 8(2), pp. 141-171.
    • (2005) Wind Energy , vol.8 , Issue.2 , pp. 141-171
    • Jackson, K.1    Zuteck, M.2    Van Dam, C.P.3    Standish, K.J.4    Berry, D.5
  • 5
    • 0346361841 scopus 로고    scopus 로고
    • Roughness sensitivity considerations for thick rotor blade airfoils
    • Van Rooij, R. P. J. O. M., and Timmer, W. A., 2003, "Roughness Sensitivity Considerations for Thick Rotor Blade Airfoils," ASME J. Sol. Energy Eng., 125(4), pp. 468-478.
    • (2003) ASME J. Sol. Energy Eng. , vol.125 , Issue.4 , pp. 468-478
    • Van Rooij, R.P.J.O.M.1    Timmer, W.A.2
  • 7
    • 33845581024 scopus 로고    scopus 로고
    • Computational design and analysis of flatback airfoil wind tunnel experiment
    • van Dam, C. P., Mayda, E. A., and Chao, D. D., 2004, "Computational Design and Analysis of Flatback Airfoil Wind Tunnel Experiment," BSDS Part II -Task 2.1 Report.
    • (2004) BSDS Part II -Task 2.1 Report
    • Van Dam, C.P.1    Mayda, E.A.2    Chao, D.D.3
  • 11
    • 30744472165 scopus 로고    scopus 로고
    • Two-dimensional wind tunnel and computational investigation of a microtab modified S809 airfoil
    • AIAA Paper No. AIAA-2005-1186
    • Baker, J. P., Standish, K. J., and van Dam, C. P., 2005, "Two-Dimensional Wind Tunnel and Computational Investigation of a Microtab Modified S809 Airfoil," 43rd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, AIAA Paper No. AIAA-2005-1186.
    • (2005) 43rd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV
    • Baker, J.P.1    Standish, K.J.2    Van Dam, C.P.3
  • 12
    • 0004246775 scopus 로고
    • Simplified method for determination of critical height distributed roughness particles for boundary-layer transition at mach numbers from 0 to 5
    • Braslow, A. L., and Knox, E. C., 1958, "Simplified Method for Determination of Critical Height Distributed Roughness Particles for Boundary-Layer Transition at Mach Numbers from 0 to 5," NACA TN 4363.
    • (1958) NACA TN , vol.4363
    • Braslow, A.L.1    Knox, E.C.2
  • 20
    • 33845369529 scopus 로고    scopus 로고
    • Bubble-induced unsteadiness on a wind turbine airfoil
    • Mayda, E. A., and van Dam, C. P., 2002, "Bubble-Induced Unsteadiness on a Wind Turbine Airfoil," ASME J. Sol. Energy Eng., 124(4), pp. 335-344.
    • (2002) ASME J. Sol. Energy Eng. , vol.124 , Issue.4 , pp. 335-344
    • Mayda, E.A.1    Van Dam, C.P.2
  • 21
    • 0028486598 scopus 로고
    • Two-equation eddy-viscosity turbulence models for engineering applications
    • Menter, F. R., 1994, "Two-Equation Eddy-Viscosity Turbulence Models for Engineering Applications," AIAA J., 32(8), pp. 1598-1605.
    • (1994) AIAA J. , vol.32 , Issue.8 , pp. 1598-1605
    • Menter, F.R.1
  • 22
    • 0032205453 scopus 로고    scopus 로고
    • Recent experience with different turbulence models applied to the calculation of flow over aircraft components
    • Kral, L. D., 1998, "Recent Experience with Different Turbulence Models Applied to the Calculation of Flow Over Aircraft Components," Prog. Aerosp. Sci., 34(7-8), pp. 481-541.
    • (1998) Prog. Aerosp. Sci. , vol.34 , Issue.7-8 , pp. 481-541
    • Kral, L.D.1
  • 26
    • 84995393926 scopus 로고
    • Integral boundary layer formulation for blunt trailing edges
    • AIAA Paper No. AIAA-1989-2166
    • Drela, M., 1989, "Integral Boundary Layer Formulation for Blunt Trailing Edges," 7th Applied Aerodynamics Conference, Seattle, July-Aug., AIAA Paper No. AIAA-1989-2166.
    • (1989) 7th Applied Aerodynamics Conference, Seattle, July-Aug.
    • Drela, M.1
  • 28
    • 34250809071 scopus 로고    scopus 로고
    • Computational fluid dynamics of flatback airfoils for wind turbine applications
    • AIAA Paper No. AIAA-2006-0194
    • Tebo, S., and Duque, E. P. N., 2006, "Computational Fluid Dynamics of Flatback Airfoils for Wind Turbine Applications," 44th AIAA Aerospace Sciences Meeting and Exhibit, Reno, AIAA Paper No. AIAA-2006-0194.
    • (2006) 44th AIAA Aerospace Sciences Meeting and Exhibit, Reno
    • Tebo, S.1    Duque, E.P.N.2
  • 31
    • 0033715429 scopus 로고    scopus 로고
    • Detached-eddy simulations past a circular cylinder
    • Travin, A., Shur, M., Strelets, M., and Spalart, P. R., 2000, "Detached-Eddy Simulations Past a Circular Cylinder," Flow, Turbul. Combust., 63(1), pp. 293-313.
    • (2000) Flow, Turbul. Combust. , vol.63 , Issue.1 , pp. 293-313
    • Travin, A.1    Shur, M.2    Strelets, M.3    Spalart, P.R.4


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.