Pressure-distribution Measurements of a Low-drag Airfoil with Slotted Flap Submitted by Curtiss-Wright Corporation
Ira H. Abbott
Jan 1941 · National Advisory Committee for Aeronautics
Ebook
2
Pages
About this ebook
The model represented a wing section of the P-60A airplane. The model was equipped with a 0.25c slotted flap with the lip on the upper airfoil surface at approximately 90 percent of the airfoil chord. The model was equipped with pressure-distribution orifices.
The model represented a wing section of the P-60A airplane. The model was equipped with a 0.25c slotted flap with the lip on the upper airfoil surface at approximately 90 percent of the airfoil chord. The model was equipped with pressure-distribution orifices.
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