Theoretical pressure distributions and lift, drag, and pitching moment characteristics at three values of Reynolds number presented for group of airfoil sections modified for high speed applications; effectiveness of flaps and effect of standard leading edge roughness also investigated at one value of Reynolds number.
Aerodynamic characteristics of number of modified NACA four-digit-series airfoil sections
Nat Advisory Committee Aeronautics -- Tech Note
1948
37 pages
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English
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