THE EFFECT OF THE SPLIT NACA 0015 AIRFOIL ON VARIATIONS IN REYNOLDS NUMBER
This research will discuss the advantages of a NACA 0015 airfoil with a split configuration under varying Reynolds numbers. Computational Fluid Dynamics (CFD) simulations with a K-epsilon turbulence model were conducted on a two-dimensional split airfoil to achieve this goal. Initially, simulations...
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Main Author: | Muhammad Fari Satria, (Author) |
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Format: | Book |
Published: |
TURBO : Jurnal Program Studi Teknik Mesin,
2023-12-31.
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Online Access: | Link Metadata |
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