Technical notes. 2251. Effects of Mach number up to 0.34 and Reynolds number up to 8X104 on maximum lift coefficient of wing of NACA 66-series airfoil sections [with list of references]; by G. Chester Furlong and James E. Fitzpatrick.
Publication Title:
Effects of Mach number up to 0.34 and Reynolds number up to 8X104 on maximum lift coefficient of wing of NACA 66-series airfoil sections [with list of references]; by G. Chester Furlong and James E. Fitzpatrick.
Display Title:
Technical notes. 2251. Effects of Mach number up to 0.34 and Reynolds number up to 8X104 on maximum lift coefficient of wing of NACA 66-series airfoil sections [with list of references]; by G. Chester Furlong and James E. Fitzpatrick.
Series Title:
Technical notes.
Corporate Agency Authors:
National Advisory Committee for Aeronautics
Sort Author:
National Advisory Committee for Aeronautics
Authors:
Furlong, G. Chester and Fitzpatrick, James E.
Date:
Dec. 1950
Publish Date ISO Format:
1950-12-01T00:00:00Z
Publication Start:
19501201
Publication End:
19501231
Corporate/Agency Author:
National Advisory Committee for Aeronautics
Publication month:
1
Publication year:
1950
Publication place:
Washington
SuDoc number:
Y 3.N 21/5:6/(nos.)
Description:
cover title, 43+[4] p. il. 4°
Notes:
[Processed.]
Notes:
[Processed.] † Distribution Made by Issuing Office.