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Information Journal Paper

Title

STATIC SURFACE PRESSURE MEASUREMENT ON A SECTION OF A WIND TURBINE BLADE

Pages

  59-65

Abstract

 An extensive experimental investigation has been conducted to study the aerodynamic behavior of a WIND TURBINE blade. A three dimensional wing was fabricated using the existing WIND TURBINE blade cross section. The wing was tested at angles of attack of -5 to 25 degrees and at various Reynolds numbers in the Shiraz subsonic WIND TUNNEL. Experimental results, such as static PRESSURE DISTRIBUTION, LIFT COEFFICIENT, WAKE and 3-D flow effects, are compared with the 2-D test results. The comparison shows that 3-D flow effects reduce both wing LIFT COEFFICIENT and blade performance, with respect to the 2-D results, while the stall angle increases considerably.

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    APA: Copy

    SOLTANI, M.R., POULI BABAEI MAMEGHANI, A., & BAKHSH ALIPOUR, A.. (2008). STATIC SURFACE PRESSURE MEASUREMENT ON A SECTION OF A WIND TURBINE BLADE. SHARIF: CIVIL ENINEERING, 24(42), 59-65. SID. https://sid.ir/paper/127993/en

    Vancouver: Copy

    SOLTANI M.R., POULI BABAEI MAMEGHANI A., BAKHSH ALIPOUR A.. STATIC SURFACE PRESSURE MEASUREMENT ON A SECTION OF A WIND TURBINE BLADE. SHARIF: CIVIL ENINEERING[Internet]. 2008;24(42):59-65. Available from: https://sid.ir/paper/127993/en

    IEEE: Copy

    M.R. SOLTANI, A. POULI BABAEI MAMEGHANI, and A. BAKHSH ALIPOUR, “STATIC SURFACE PRESSURE MEASUREMENT ON A SECTION OF A WIND TURBINE BLADE,” SHARIF: CIVIL ENINEERING, vol. 24, no. 42, pp. 59–65, 2008, [Online]. Available: https://sid.ir/paper/127993/en

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