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## README
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#About the software
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## About the software
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# What is it for?
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## What is it for?
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Wind turbines and propellers involve relatively complex geometries, and due to the rotation of the turbine, movement of the air, and the fact that lift is a function of the shape of each blade, it is hard to calculate the forces, power and efficiency of such systems by hand.
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Methods for determining the parameters of such turbines were in the past mainly experimental, and nowadays relatively accurate calculations can be made using 3D computational fluid dynamics calculations. The main disadvantages to such methods are the cost, and time involved in preparation, calculation, and post-calculation analysis.
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In order for a turbine designer to quickly generate a geometry and determine the forces and other parameters of a turbine, a fast, cost-effective way is to use the blade element momentum theory.
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# Blade element momentum theory
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##Blade element momentum theory
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Blade Element Momentum theory software (BEM) is a tool for calculating the local forces on a propeller or wind turbine using the blade element momentum theory. The calculation is based on the Rankine-Froude momentum theory and the blade element theory.
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c. (optionally) statical analysis
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d. other parameters
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# Similar software
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##Similar software
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Software that fulfill a similar role, and were an inspiration to the development of this software, include:
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QBlade, Aerodyn, XFOIL, etc.
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## How to use the software
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# Main window
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###Main window
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The BEM software main window is divided into multiple tabs, which are divided by their corresponding function, these are: Airfoil management, Turbine info, Analysis and Optimization. The analysis is started on the Analyiss tab and after it is finished, an Results window is finally opened, from which results can be checked on and exported, as necessary.
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# Airfoil management
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###Airfoil management
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In the Airfoil management tab, a designer can:
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a. Add, rename, duplicate, remove, load and save airfoil data
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b. import airfoil data
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c. import or calculate the cL/cD curves of an airfoil
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d. create 360° cL/cD curves using Montgomerie methods
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# Turbine info
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###Turbine info
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In the Turbine info tab, a designer can:
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a. Set up the basic turbine data (name, radii, number of blades, etc.)
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e. Export the geometry to Solidworks
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f. Create standard geometry graphs for distribution and documentation purposes
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# Analysis
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###Analysis
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In the Analysis tab, a designer can:
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a. Determine the basic calculation parameters
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b. Run the analysis, which will, after finishing, open the results window
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# Optimization
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###Optimization
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In the Optimization tab, the designer can optimize the geometry using an optimization algorithm in order to ensure that the geometry is optimized to a specific fluid speed/rotational velocity combination. The parameters that will be modified are called input parameters, and the parameters that will determine the success of the optimization (optimization function) are called the output variables. Target variables are also supported, in case one desires not the largest torque, power, or other parameter, but instead a specific torque, power or other parameter.
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