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Old 01-16-2012, 12:31 PM
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Default Aerodynamic Characteristics Of The Naca 8-H-12 Airfoil At Six Reynolds Numbers
report: naca-tn-1998
title: Aerodynamic Characteristics Of The Naca 8-H-12 Airfoil Section At Six Reynolds Numbers From 1.8 x E6 TO 11.0 x E6
author: By Raymond F. Schaefer, Hamilton A. Smith
http://ia700609.us.archive.org/14/it...9930082712.pdf
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