A range of aerodynamic analyses are introduced to enable the initial spreadsheet calculations to be refined. These are chiefly based on the panel codes XFoil and XFLR5 and the RANS CFD code Fluent. Depending on the sophistication and budget of the design team, this process can be quite lightweight or can involve significant computational runs.


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    Title :

    Preliminary Aerodynamic and Stability Analysis


    Contributors:


    Publication date :

    2017-10-23


    Size :

    41 pages




    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




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