1949•Unpublished venueRequires access
Aerodynamic Characteristics of the NACA 8-H-12 Airfoil Section at Six Reynolds Numbers from 1.8 x 10(exp 6) to 11.0 x 10(exp 6).
Raymond F Schaefer, Hamilton A Smith
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Abstract
Report presenting an investigation in the two-dimensional low-turbulence pressure tunnel to determine the aerodynamic characteristics of the NACA 8-H-12 airfoil section at four Reynolds numbers. The section lift, drag, and pitching-moment characteristics are presented for smooth and rough surface conditions. Generally, no unusual scale effects are present for either condition.