Technical notes. 2278. Theoretical symmetric span loading due to flap deflection for wings of arbitrary plan form at subsonic speeds [with list of references]; by John DeYoung.
Publication Title:
Theoretical symmetric span loading due to flap deflection for wings of arbitrary plan form at subsonic speeds [with list of references]; by John DeYoung.
Display Title:
Technical notes. 2278. Theoretical symmetric span loading due to flap deflection for wings of arbitrary plan form at subsonic speeds [with list of references]; by John DeYoung.
Series Title:
Technical notes.
Corporate Agency Authors:
National Advisory Committee for Aeronautics
Sort Author:
National Advisory Committee for Aeronautics
Authors:
DeYoung, John
Date:
Jan. 1951
Publish Date ISO Format:
1951-01-01T00:00:00Z
Publication Start:
19510101
Publication End:
19510131
Corporate/Agency Author:
National Advisory Committee for Aeronautics
Publication month:
12
Publication year:
1951
Publication place:
Washington
SuDoc number:
Y 3.N 21/5:6/(nos.)
Description:
cover title, 71+[6] p. il. 4°
Notes:
[Processed.]
Notes:
[Processed.] † Distribution Made by Issuing Office.