Technical notes. 3127. Effectiveness at high subsonic Mach numbers of 20-percent-chord plain trailing-edge flap on NACA 65-210 airfoil section [with list of references]; by Louis S. Stivers, jr.
Publication Title:
Effectiveness at high subsonic Mach numbers of 20-percent-chord plain trailing-edge flap on NACA 65-210 airfoil section [with list of references]; by Louis S. Stivers, jr.
Display Title:
Technical notes. 3127. Effectiveness at high subsonic Mach numbers of 20-percent-chord plain trailing-edge flap on NACA 65-210 airfoil section [with list of references]; by Louis S. Stivers, jr.
Series Title:
Technical notes.
Corporate Agency Authors:
National Advisory Committee for Aeronautics
Sort Author:
National Advisory Committee for Aeronautics
Authors:
Stivers, Louis S. jr.
Date:
Mar. 1954
Publish Date ISO Format:
1954-03-01T00:00:00Z
Publication Start:
19540301
Publication End:
19540331
Corporate/Agency Author:
National Advisory Committee for Aeronautics
Publication month:
10
Publication year:
1954
Publication place:
Washington
SuDoc number:
Y 3.N 21/5:6/(nos.)
Description:
cover title, 15 p.+[2] leaves, il. 4°
Notes:
[Processed. The pages or leaves in brackets in each collation consist of detachable card catalog entries.]
Notes:
[Processed. The pages or leaves in brackets in each collation consist of detachable card catalog entries.] † Distribution Made by Issuing Office.