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Universitas Hasanuddin
Research output:Contribution to journal›Article›peer-review
Aerodynamic Performance of Swayasa Aircraft Wing Model against the Effect of Airfoil Flap Angle Configuration
Salam N.
International Journal of Mechanical Engineering and Robotics Research
Q3Published: 2025
Abstract
Sourced directly from Elsevier Scopus. No OpenAlex abstract available.
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10.18178/IJMERR.14.1.48-58Other files and links
- Link to publication in Scopus
- Open Access Version Available
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AirfoilSciences
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