Technical notes. 3174. Influence of airfoil trailing-edge angle and trailing-edge-thickness variation on effectiveness of plain flap at high subsonic Mach numbers [with list of references]; by Albert D. Hemenover and Donald J. Graham.
Publication Title:
Influence of airfoil trailing-edge angle and trailing-edge-thickness variation on effectiveness of plain flap at high subsonic Mach numbers [with list of references]; by Albert D. Hemenover and Donald J. Graham.
Display Title:
Technical notes. 3174. Influence of airfoil trailing-edge angle and trailing-edge-thickness variation on effectiveness of plain flap at high subsonic Mach numbers [with list of references]; by Albert D. Hemenover and Donald J. Graham.
Series Title:
Technical notes.
Corporate Agency Authors:
National Advisory Committee for Aeronautics
Sort Author:
National Advisory Committee for Aeronautics
Authors:
Hemenover, Albert D. and Graham, Donald J.
Date:
June 1954
Publish Date ISO Format:
1954-06-01T00:00:00Z
Publication Start:
19540601
Publication End:
19540630
Corporate/Agency Author:
National Advisory Committee for Aeronautics
Publication month:
7
Publication year:
1954
Publication place:
Washington
SuDoc number:
Y 3.N 21/5:6/(nos.)
Description:
cover title, 101 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.]