SIMULATION-BASED ANALYSIS OF AERODYNAMIC PROPERTIES OF NACA 2412 AIRFOIL WITH ADDITIONAL FLAP AND SLAT ELEMENTS
The original concept for the Easy-Fly project was to create an ultra-light STOL (Short Takeoff and Landing) plane featuring minimal drag and speed attributes. To support this goal, CFD (Computational Fluid Dynamics) was applied by varying the configuration of single-grooved flaps and slats and the a...
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| Autori principali: | , , , , , |
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| Natura: | Artigo |
| Lingua: | Inglês |
| Pubblicazione: |
Program Studi Teknik Mesin, Universitas Lambung Mangkurat
2025-10-01
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| Serie: | Scientific Journal of Mechanical Engineering Kinematika |
| Soggetti: | |
| Accesso online: | https://kinematika.ulm.ac.id/index.php/kinematika/article/view/724 |
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