Numerical Study on Single and Multi-Element NACA 43018 Wing Airfoil with Leading-Edge Slat and Slotted Flap.

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Bibliographic Details
Title: Numerical Study on Single and Multi-Element NACA 43018 Wing Airfoil with Leading-Edge Slat and Slotted Flap.
Authors: S. P., Setyo Hariyadi1,2, setyo_hariyadi@poltekbangsby.ac.id, Pitoyo, Bambang Juni1, Pambudiyatno, Nyaris3, Sutardi4, Widodo, Wawan Aries4
Source: International Journal of Automotive & Mechanical Engineering; Sep2024, Vol. 21 Issue 3, p11652-11662, 11p
Database: Applied Science & Technology Source
Description
ISSN:22298649
DOI:10.15282/ijame.21.3.2024.16.0899