NACA research memorandum RM (series). L58E06. Effects of wing sweep, horizontal-tail configuration, and ventral fin on static stability characteristics of model with wing of aspect ratio 3 at Mach nos. from 2.29 to 4.65 [with list of references]; by Byron M. Jaquet and Roger H. Fournier.
Publication Title:
Effects of wing sweep, horizontal-tail configuration, and ventral fin on static stability characteristics of model with wing of aspect ratio 3 at Mach nos. from 2.29 to 4.65 [with list of references]; by Byron M. Jaquet and Roger H. Fournier.
Display Title:
NACA research memorandum RM (series). L58E06. Effects of wing sweep, horizontal-tail configuration, and ventral fin on static stability characteristics of model with wing of aspect ratio 3 at Mach nos. from 2.29 to 4.65 [with list of references]; by Byron M. Jaquet and Roger H. Fournier.
Series Title:
NACA research memorandum RM (series).
Corporate Agency Authors:
National Aeronautics and Space Administration
Sort Author:
National Aeronautics and Space Administration
Authors:
Jaquet, Byron M. and Fournier, Roger H.
Date:
Washington, July 21, 1958
Publish Date ISO Format:
1958-07-21T00:00:00Z
Publication Start:
19580721
Publication End:
19580721
Corporate/Agency Author:
National Aeronautics and Space Administration
Publication month:
6
Publication year:
1958
SuDoc number:
Y 3.N 21/5:15/(letter-nos.)
Description:
cover title, 83+[6] p. il. 4°
Notes:
(National Advisory Committee for Aeronautics.) [Processed. No longer confidential. Classification changed Jan. 12, 1961.]
Notes:
(National Advisory Committee for Aeronautics.) [Processed. No longer confidential. Classification changed Jan. 12, 1961.] † Distribution Made by Issuing Office.