Airfoil family suitable for 5-10 mw wind turbine blades
A wind turbine blade, NPU-MWA-210 technology, applied in the field of blade airfoil design, can solve the problems of low design Reynolds number and unsuitable for multi-megawatt large wind turbine blades, etc.
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experiment example 1
[0097]The inventor calculated the aerodynamic performance of the NPU-MWA airfoil family of the present invention using the Reynolds-averaged Navier-Stokes method (RANS), respectively adopted the free transition calculation and the full turbulence calculation, and the calculation results are shown in Table 10. The design of the airfoil The lift coefficients are all over 1.2. The section moments of inertia in Table 10 are calculated under the assumption that the airfoil chord length is 1m.
[0098] Table 10 Main aerodynamic characteristics of NPU-MWA multi-megawatt wind turbine airfoil family
[0099]
experiment example 2
[0101] This experimental example is used to compare the difference in aerodynamic performance between the NPU-MWA-180 airfoil and the similar comparison airfoil.
[0102] Specifically, the NPU-MWA-180 airfoil disclosed by the present invention is used as the design airfoil, and the NPU-WA airfoil and DU airfoil with the same relative thickness are used as the comparison airfoil, namely: DU96-W-180 airfoil and NPU -WA-180 airfoil is a comparative airfoil. Among them, the DU96-W-180 airfoil is an airfoil with a relative thickness of 0.18 designed by Delft University in the Netherlands; the reference "Design of Airfoils for Wind Turbine Blades", the link is https: / / gcep.stanford.edu / pdfs / energy_workshops_04_04 / wind_van_rooij.pdf ; The NPU-WA-180 airfoil is an airfoil with a relative thickness of 0.18 disclosed by the patent application number CN201110023215.1.
[0103] The inventor used airfoil aerodynamic analysis software to compare and calculate the aerodynamic performanc...
experiment example 3
[0105] This experimental example is used to compare the difference in aerodynamic performance between the NPU-MWA-210 airfoil and the similar comparison airfoil.
[0106] Specifically, the NPU-MWA-210 airfoil disclosed by the present invention is used as the design airfoil, and the NPU-WA airfoil and DU airfoil with the same relative thickness are used as the comparison airfoil, namely: DU93-W-210 airfoil and NPU -WA-210 airfoil is a comparative airfoil. Among them, the DU93-W-210 airfoil is an airfoil with a relative thickness of 0.21 designed by Delft University in the Netherlands; the reference is Denmark "Wind Turbine Airfoil Catalogue" published by the National Laboratory in 2001, the link is http: / / orbit.dtu.dk / files / 7728949 / ris_r_1280.pdf ; The NPU-WA-210 airfoil is an airfoil with a relative thickness of 0.21 disclosed in the invention patent with the patent application number CN201110023215.1.
[0107] The inventor used airfoil aerodynamic analysis software to ...
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