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.
Sensitivity Analysis and Optimization for a Trainer Aircraft Configuration
Lect.Notes Mechanical Engineering
National Conference on Multidisciplinary Analysis and Optimization ; 2021 October 07, 2021 - October 09, 2021
2022-09-25
6 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
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