Geometry modification of a trainer aircraft using drag sensitivities is presented. Wing shape optimization has been carried out using the open source tool SU2. An overall drag reduction of around 72 counts for the full aircraft with sensitivity analysis is achievedÅ. Further wing shape optimization resulted in a 28 count reduction in the drag.


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    Title :

    Sensitivity Analysis and Optimization for a Trainer Aircraft Configuration


    Additional title:

    Lect.Notes Mechanical Engineering



    Conference:

    National Conference on Multidisciplinary Analysis and Optimization ; 2021 October 07, 2021 - October 09, 2021



    Publication date :

    2022-09-25


    Size :

    6 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




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