Technical notes. 2753. Effects of Mach number variation between 0.07 and 0.34 and Reynolds number variation between 0.97×106 and 8.10×106 on maximum lift coefficient of wing of NACA 64-210 airfoil sections [with list of references]: by James E. Fitzpatrick and William C. Schneider.
Publication Title:
Effects of Mach number variation between 0.07 and 0.34 and Reynolds number variation between 0.97×106 and 8.10×106 on maximum lift coefficient of wing of NACA 64-210 airfoil sections [with list of references]: by James E. Fitzpatrick and William C. Schneider.
Display Title:
Technical notes. 2753. Effects of Mach number variation between 0.07 and 0.34 and Reynolds number variation between 0.97×106 and 8.10×106 on maximum lift coefficient of wing of NACA 64-210 airfoil sections [with list of references]: by James E. Fitzpatrick and William C. Schneider.
Series Title:
Technical notes.
Corporate Agency Authors:
National Advisory Committee for Aeronautics
Sort Author:
National Advisory Committee for Aeronautics
Authors:
Fitzpatrick, James E. and Schneider, William C.
Date:
Aug. 1952
Publish Date ISO Format:
1952-08-01T00:00:00Z
Publication Start:
19520801
Publication End:
19520831
Corporate/Agency Author:
National Advisory Committee for Aeronautics
Publication month:
5
Publication year:
1952
Publication place:
Washington
SuDoc number:
Y 3.N 21/5:6/(nos.)
Description:
cover title, 34 p.+[3] leaves, il. 4°
Notes:
[Processed.]
Notes:
[Processed.] † Distribution Made by Issuing Office.