Russ. Aeronaut.
 2023
DOI: 10.3103/s1068799823040190
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Cessna 172 G1000 Aircraft Airfoil Optimization Using Particle Swarm Optimization Method Applying a Direct Airfoil Design Approach to Obtain the Maximum Lift-to-Drag Ratio

Dinku Seyoum Zeleke,
Abdurehman Yimer Asfaw,
Bethel Lemma Bizuneh
et al.
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