NACA research memorandum RM (series). L56L18. Free-flight experience of lateral stability characteristics at low lift of 45° swept-wing rocket-propelled model equipped with nonlinear yaw-rate damper system at Mach numbers from 0.76 to 1.73 [with list of references]; by Charles T. D'Aiutolo, William W. Willoughby, and Lucille C. Coltrane.
Publication Title:
Free-flight experience of lateral stability characteristics at low lift of 45° swept-wing rocket-propelled model equipped with nonlinear yaw-rate damper system at Mach numbers from 0.76 to 1.73 [with list of references]; by Charles T. D'Aiutolo, William W. Willoughby, and Lucille C. Coltrane.
Display Title:
NACA research memorandum RM (series). L56L18. Free-flight experience of lateral stability characteristics at low lift of 45° swept-wing rocket-propelled model equipped with nonlinear yaw-rate damper system at Mach numbers from 0.76 to 1.73 [with list of references]; by Charles T. D'Aiutolo, William W. Willoughby, and Lucille C. Coltrane.
Series Title:
NACA research memorandum RM (series).
Corporate Agency Authors:
National Aeronautics and Space Administration
Sort Author:
National Aeronautics and Space Administration
Authors:
D'Aiutolo, Charles T., Willoughby, William W., and Coltrane, Lucille C.
Date:
Feb. 8, 1957
Publish Date ISO Format:
1957-02-08T00:00:00Z
Publication Start:
19570208
Publication End:
19570208
Corporate/Agency Author:
National Aeronautics and Space Administration
Publication month:
11
Publication year:
1957
Publication place:
Washington
SuDoc number:
Y 3.N 21/5:15/(letter-nos.)
Description:
cover title, 57+[6] p. il. 4°
Notes:
[No longer confidential. Classification changed Feb. 10, 1959.] and (National Advisory Committee for Aeronautics.) [Processed. The pages or leaves in brackets in each collation consist of detachable card catalog entries.]
Notes:
(National Advisory Committee for Aeronautics.) [Processed. The pages or leaves in brackets in each collation consist of detachable card catalog entries.] † Distribution Made by Issuing Office.