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CHAPTER 2 Basic Theory for Wind Turbine Blade Aerodynamics

By continuity equation, rrvA vA 11 2 2= . (2) Thus, eqn (2) yields as =r ( ) 22 − 11 1 2 1. 2 P vA v v (3) Figure 1: Actuator disc and stream tube [1] www.witpress.com, ISSN 1755-8336 (on-line) WIT Transactions on State of the Art in Science and Engineering, Vol 81, ©2014 WIT Press

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Transcription of CHAPTER 2 Basic Theory for Wind Turbine Blade Aerodynamics

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