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Aerodynamic characteristics at Reynolds numbers of 3.0 x 10⁶ and 6.0 x 10⁶ of three airfoil sections formed by cutting off various amounts from the rear portion of the NACA 0012 airfoil section
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Aerodynamic characteristics at Reynolds numbers of 3.0 x 10⁶ and 6.0 x 10⁶ of three airfoil sections formed by cutting off various amounts from the rear portion of the NACA 0012 airfoil section
ID:
3469532
Creatori:
(1401175) Smith Hamilton A.
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