Perubahan Distribusi Tekanan Aerofoil Akibat Pengaruh Variasi Sudut Serang

Syamsul Hadi

Abstract


Abstract : This study aims to measurements pressure distributions caused to angle of attack variations. NACA 0012 airfoils were tested in low speed wind tunnel at 100-160 angle of attack and Reynolds number variations. The result of the research showed pressure distributions characteristics. Stall happened at 120-160 angle of attack.

Key words: dihedral angle, airfoil, low speed wind-tunnel


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Mekanika: Majalah Ilmiah Mekanika

ISSN: 1412-7962 || eISSN: 2579-3144

Address :  Jl. Ir Sutami no 36 A, Building I, Faculty of Engineering, Universitas Sebelas Maret, Surakarta.

Phone    :  +62271632163 

email     : mesin@ft.uns.ac.id

 

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