# Aerodynamic Performance of Swayasa Aircraft Wing Model against the Effect of Airfoil Flap Angle Configuration
> Salam N.

URL kanonis: https://discover.unhas.ac.id/publications/aerodynamic-performance-of-swayasa-aircraft-wing-model-against-the-effect-of-air
Jurnal / Konferensi: International Journal of Mechanical Engineering and Robotics Research
Tahun terbit: 2025
DOI: https://doi.org/10.18178/IJMERR.14.1.48-58
ISSN: 22780149
Kuartil SJR: Q3
Citations: 0

## Authors
- Salam N.

## Abstract
Sourced directly from Elsevier Scopus. No OpenAlex abstract available.

## Keywords
- Airfoil
- Wing
- Aerodynamics
- Angle of attack
- Aerospace engineering
- Wing configuration
- Wing twist
- Structural engineering
- Engineering
- Marine engineering

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Sumber: Discover Unhas — RIMS Universitas Hasanuddin.
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