1976
DOI: 10.2172/7269797
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Wind tunnel performance data for the Darrieus wind turbine with NACA 0012 blades

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1978
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Cited by 73 publications
(37 citation statements)
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“…[18] the chord Reynolds number ranges from 1 Â 10 5 to 3 Â 10 5 ), nor to a different solidity (which, again, is here comparable to the one in Ref. [18]). On the other hand, such difference could be connected with higher stall characteristics of the DU-06-W200 airfoil (characterized by a thickness to chord ratio of 0.18) with respect to the NACA 0012 one (adopted in Ref.…”
Section: Normalized Powersupporting
confidence: 76%
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“…[18] the chord Reynolds number ranges from 1 Â 10 5 to 3 Â 10 5 ), nor to a different solidity (which, again, is here comparable to the one in Ref. [18]). On the other hand, such difference could be connected with higher stall characteristics of the DU-06-W200 airfoil (characterized by a thickness to chord ratio of 0.18) with respect to the NACA 0012 one (adopted in Ref.…”
Section: Normalized Powersupporting
confidence: 76%
“…12, it can be argued that the negative C Paero band at low TSR eq s could be very small. In other words, extrapolating the proposed measurements to low TSR eq values, the C Paero could be not so small as that obtained during Sandia tests on small VAWTs [18]. Moreover, comparing the C Paero -TSR eq curve at 200 rpm (chord Reynolds number of 1.4 Â 10 5 ) to the one at 300 rpm (chord Reynolds number of 2.5 Â 10 5 ), it clearly appears that the local (i.e.…”
Section: Normalized Powermentioning
confidence: 52%
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“…Rigorous and exhaustive experimental data from both wind tunnel and field measurements for different sizes of VAWTs were collected by these institutes in the 1970s and 1980s [3][4][5][6][7][8]. These experiments and other wind tunnel and field measurements, which were done during those years [9][10][11][12][13][14], mainly focused on overall rotor performance (e.g., power and torque) and loading on the blades.…”
Section: Introductionmentioning
confidence: 99%
“…These results can be used to design low-noise Savonius wind turbines. (1) . Fujisawa는 유동가시화 실험 및 날개 위에서의 압력 측정 실험을 통해 사보 니우스 풍력발전기의 토크 생성 메커니즘을 실험적 으로 밝혀내었다 (2) .…”
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