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    Experimental Analysis of a NACA 0021 Airfoil Section Through 180-Deg Angle of Attack at Low Reynolds Numbers for Use in Wind Turbine Analysis 

    Source: Journal of Engineering for Gas Turbines and Power:;2019:;volume( 141 ):;issue: 004:;page 41012
    Author(s): Holst, D.; Church, B.; Pechlivanoglou, G.; Tüzüner, E.; Saverin, J.; Nayeri, C. N.; Paschereit, C. O.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Wind turbine industry has a special need for accurate post stall airfoil data. While literature often covers incidence ranges [−10 deg, +25 deg], smaller machines experience a range of up to 90 deg for horizontal axis and ...
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    Experimental Analysis of a NACA 0021 Airfoil Under Dynamic Angle of Attack Variation and Low Reynolds Numbers 

    Source: Journal of Engineering for Gas Turbines and Power:;2019:;volume( 141 ):;issue: 003:;page 31020
    Author(s): Holst, D.; Church, B.; Wegner, F.; Pechlivanoglou, G.; Nayeri, C. N.; Paschereit, C. O.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The wind industry needs reliable and accurate airfoil polars to properly predict wind turbine performance, especially during the initial design phase. Medium- and low-fidelity simulations directly depend on the accuracy ...
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