Experimental Study on the Aerodynamic Performance of Swept Curved Blade
نویسندگان
چکیده
منابع مشابه
Low - Speed Theoretical and Experimental Aerodynamic Loading on Highly - Swept Curved - Tipped Wings of Two Thicknesses
An approximate theoretical formula for the distribution of aerodynamic load over arbitrary thick wings in incompressible flow is developed by combining three-dimensional results from thin-wing theory with two-dimensional results from thick-aerofoil theory. The formula is applied to two wings of identical planform, with 60 degrees trailing-edge sweepback and differing aerofoil thickness, which h...
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ژورنال
عنوان ژورنال: Chinese Journal of Aeronautics
سال: 2004
ISSN: 1000-9361
DOI: 10.1016/s1000-9361(11)60227-6