Technical notes. 2831. Span load distributions resulting from constant angle of attack, steady rolling velocity, steady pitching velocity, and constant vertical acceleration for tapered sweptback wings with streamwise tips, subsonic leading edges and supersonic trailing edges [with list of references]; by Margery E. Hannah and Kenneth Margolis.
Publication Title:
Span load distributions resulting from constant angle of attack, steady rolling velocity, steady pitching velocity, and constant vertical acceleration for tapered sweptback wings with streamwise tips, subsonic leading edges and supersonic trailing edges [with list of references]; by Margery E. Hannah and Kenneth Margolis.
Display Title:
Technical notes. 2831. Span load distributions resulting from constant angle of attack, steady rolling velocity, steady pitching velocity, and constant vertical acceleration for tapered sweptback wings with streamwise tips, subsonic leading edges and supersonic trailing edges [with list of references]; by Margery E. Hannah and Kenneth Margolis.
Series Title:
Technical notes.
Corporate Agency Authors:
National Advisory Committee for Aeronautics
Sort Author:
National Advisory Committee for Aeronautics
Authors:
Hannah, Margery E. and Margolis, Kenneth
Date:
Dec. 1952
Publish Date ISO Format:
1952-12-01T00:00:00Z
Publication Start:
19521201
Publication End:
19521231
Corporate/Agency Author:
National Advisory Committee for Aeronautics
Publication month:
1
Publication year:
1952
Publication place:
Washington
SuDoc number:
Y 3.N 21/5:6/(nos.)
Description:
cover title, 221+[6] p. il. 4°
Notes:
[Processed.]
Notes:
[Processed.] † Distribution Made by Issuing Office.