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How to Design Wind Turbine Blade Geometry for Optimal Aerodynamic Efficiency

This is part 3 of my series: “How Does a Wind Turbine Work?” In this video I show you how to use the blade element momentum theory, BEM, that we discussed in the last videos, to design an efficient wind turbine rotor. Topics include: 00:33 Lift equation 00:47 Optimum aerodynamic conditions with constant circulation along the span 01:05 How the local wind speed and angle vary along the length of the blade 01:22 How to change the chord and twist angle along the blade span 01:50 Why designers normally modify the chord distribution to have smaller chords at the root 02:28 The torque equation and why the tip's aerodynamics is more important than the root 02:52 What happens if you use a turbine at a different wind speed than it was designed for 03:46 How variable speed turbines can operate efficiently over a wind range of wind speeds 04:18 What is tip speed ratio (TSR) and why is it important to wind turbine designers? 04:48 Blade solidity 06:07 How to find a starting point in the wind turbine blade design process 07:22 Why are wind turbine blades getting so skinny? 07:54 Reducing wind turbine noise by limiting rotational speed 08:29The different requirements of aerofoils at the root versus tip of the blade Check out part one and two of my “How Does a Wind Turbine Work?” series where I go through the mechanical engineering and aerodynamic theory needed to understand how a wind turbine works and design a wind turbine blade: How Much Energy is in the Wind?    • The Betz Limit in Wind Turbines   How to Calculate Wind Turbine Power Output: Blade Element Momentum Method    • How to Calculate Wind Turbine Power O...   If you want to follow the derivations I mentioned in this video then check out section 3.7.2 of Burton's "Wind Energy Handbook." Available to buy from Amazon (affiliate link), or your university library probably has it! https://amzn.to/32Pb1fh The optimum aerodynamic design equation at 6:10 has the following parameters: sigma_r = chord solidity at the radial location (chord length divided by swept circumference at that radial location) lambda = tip speed ratio (tip speed due to blade rotation (radial location times rotational speed) divided by wind speed) C_l = local lift coefficient mu = r/R (radial location divided by radius)