Technical notes. 2298. Modification to thin-airfoil-section theory, applicable to arbitrary airfoil sections, to account for effects of thickness on lift distribution [with list of references]; by David Graham.
Publication Title:
Modification to thin-airfoil-section theory, applicable to arbitrary airfoil sections, to account for effects of thickness on lift distribution [with list of references]; by David Graham.
Display Title:
Technical notes. 2298. Modification to thin-airfoil-section theory, applicable to arbitrary airfoil sections, to account for effects of thickness on lift distribution [with list of references]; by David Graham.
Series Title:
Technical notes.
Corporate Agency Authors:
National Advisory Committee for Aeronautics
Sort Author:
National Advisory Committee for Aeronautics
Authors:
Graham, David
Date:
Feb. 1951
Publish Date ISO Format:
1951-02-01T00:00:00Z
Publication Start:
19510201
Publication End:
19510228
Corporate/Agency Author:
National Advisory Committee for Aeronautics
Publication month:
11
Publication year:
1951
Publication place:
Washington
SuDoc number:
Y 3.N 21/5:6 (nos.)
Description:
cover title, 17+[2] p. il. 4°
Notes:
[Processed.]
Notes:
[Processed.] † Distribution Made by Issuing Office.