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[in Japanese]
2006 Volume 30 Issue 2 Pages
3
Published: 2006
Released on J-STAGE: January 27, 2011
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[in Japanese]
2006 Volume 30 Issue 2 Pages
6-11
Published: 2006
Released on J-STAGE: January 27, 2011
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[in Japanese]
2006 Volume 30 Issue 2 Pages
12-22
Published: 2006
Released on J-STAGE: January 27, 2011
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[in Japanese]
2006 Volume 30 Issue 2 Pages
23-30
Published: 2006
Released on J-STAGE: January 27, 2011
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[in Japanese], [in Japanese], [in Japanese]
2006 Volume 30 Issue 2 Pages
31-35
Published: 2006
Released on J-STAGE: January 27, 2011
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[in Japanese]
2006 Volume 30 Issue 2 Pages
36-41
Published: 2006
Released on J-STAGE: January 27, 2011
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[in Japanese]
2006 Volume 30 Issue 2 Pages
42-45
Published: 2006
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[in Japanese]
2006 Volume 30 Issue 2 Pages
46-48
Published: 2006
Released on J-STAGE: January 27, 2011
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[in Japanese]
2006 Volume 30 Issue 2 Pages
49-51
Published: 2006
Released on J-STAGE: January 27, 2011
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[in Japanese], [in Japanese], [in Japanese], [in Japanese]
2006 Volume 30 Issue 2 Pages
52-57
Published: 2006
Released on J-STAGE: January 27, 2011
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[in Japanese]
2006 Volume 30 Issue 2 Pages
58-61
Published: 2006
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[in Japanese]
2006 Volume 30 Issue 2 Pages
62-65
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Kazunori Matsumoto, Masahiro Yotsuda, Atsushi Nagata, Hironari Ogata
2006 Volume 30 Issue 2 Pages
66-70
Published: 2006
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[in Japanese]
2006 Volume 30 Issue 2 Pages
71-77
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[in Japanese]
2006 Volume 30 Issue 2 Pages
78-87
Published: 2006
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Takanori Uchida, Yuji Ohya, Tetsuya Suwabe, Graham Li
2006 Volume 30 Issue 2 Pages
101-108
Published: 2006
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1st Report, Cases When the Trailing Edge Has Zero Degree Angle
Kazumasa AMEKU, Baku M. NAGAI
2006 Volume 30 Issue 2 Pages
109-112
Published: 2006
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Wing characteristics have been analyzed for long term, however it has been scarcely described about difference of pressure distribution around the trailing edge between theories and experiments.One of the determining methods of wing characteristics is well known Kutta's condition. Kutta's condition is a method to avoid velocity infinity at the trailing edge.This paper cleared that stagnation point and singular point are simultaneously disappeared with Kutta's condition at the trailing edge using Joukowski translation.The pressure coefficient at the trailing edge has been analytically deduced as function of attack of angle, camber and wing thickness.
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Takashi KARASUDANI, Yuji OHYA, Kimihiko WATANABE
2006 Volume 30 Issue 2 Pages
113-116
Published: 2006
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We theoretically and numerically study the response of horizontal axis small wind turbines to wind-speed change.A simple model was given for a small wind turbine.Formulas for estimating a starting and a response time from a torque coefficient and the moment of inertia were presented. The estimated times agree fairly well with the times which were derived by the simulation on the model.
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1strep.City wind analysis
H. ONODERA, Y. KA-CHI, T. KAWAMURA
2006 Volume 30 Issue 2 Pages
117-122
Published: 2006
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[in Japanese]
2006 Volume 30 Issue 2 Pages
123-130
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[in Japanese]
2006 Volume 30 Issue 2 Pages
131-134
Published: 2006
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