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Let’s a consider here source:

λ Manwell = Ω 푈 푅

, J. L.F., ,Rogers. " and G.J.Anthony McGowan, Aerodynamics Aerodynamics Explained: Theory, Design and Application, Second Edition (2009 Edition Application, andDesign Second Theory, Explained: H - Darrieus

tan (i.e.turbinestraight windblades) 푈 푈 푟푒푙 훼 = 2 = 1 ( − 1 − 휆 푎

+ 푎

sin ) 8 ( cos

1 휙 − + 휙 Aerodynamics of turbines wind Aerodynamics 푎 휆

) sin of of VAWT 휙 2 + (

1 ). −

푎 ) POLI cos ." Wind EnergyWind ." - 휙 Wind ResearchWind Lab

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TSR = 2 = TSR

tan 훼 = 1 9 ( − 1

− 푎 푎 sin ) cos 휙 of of VAWT + 휙 휆

TSR = 8 = TSR POLI - Wind ResearchWind Lab

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Edition(2009). Second Theory,Explained:Windturbines."Energy wind"Aerodynamics of Application, Designand For forsee, instance,details Not covered here.  

Multiple Single 푎 solved iteratively. torqueThen computefrom get: topower 1 −

푎 Stream TubeStream

Stream TubeStream Momentum Theory = 8 퐵푐 휋푅 Aerodynamics Aerodynamics

0 2 휋

푈 Momentum Theory 푈 푟푒푙 2 Manwell 퐶 퐶 푃 퐿 cos = 4 휆 휋푅 퐵푐 훼 , J.F.,, J.AnthonyL.G. McGowan, Rogers.and +

0 휙 2 휋 + 푈

퐶 푈 푟푒푙 퐷 10 sin 2

퐶 훼 퐿 + sin 휙 of of VAWT 훼 − 푑 휙 퐶

푑 cos and 훼

푑 tan 휙

훼 POLI = - 1 Wind ResearchWind Lab (

− 1 − 푎 푎 sin ) cos 휙 + 휙 휆