Aerodynamic characteristics at Reynolds numbers of 3.0 x 10(exp 6) and 6.0 x 10(exp 6) of three airfoil sections formed by cutting off various amounts from the rear portion of the NACA 0012 airfoil section
Description: No Description Available.
Date: April 1950
Creator: Smith, Hamilton A & Schaefer, Raymond F
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department