NACA research memorandum RM (series). L56B24. Aerodynamic characteristics of 6-percent-thick symmetrical circulararc airfoil having 30-percent-chord trailing-edge flap at Mach number of 6.9 [with list of references]; by Herbert W. Ridyard and David E. Fetterman, jr.
Publication Title:
Aerodynamic characteristics of 6-percent-thick symmetrical circulararc airfoil having 30-percent-chord trailing-edge flap at Mach number of 6.9 [with list of references]; by Herbert W. Ridyard and David E. Fetterman, jr.
Display Title:
NACA research memorandum RM (series). L56B24. Aerodynamic characteristics of 6-percent-thick symmetrical circulararc airfoil having 30-percent-chord trailing-edge flap at Mach number of 6.9 [with list of references]; by Herbert W. Ridyard and David E. Fetterman, jr.
Series Title:
NACA research memorandum RM (series).
Corporate Agency Authors:
National Aeronautics and Space Administration
Sort Author:
National Aeronautics and Space Administration
Authors:
Ridyard, Herbert W. and Fetterman, David E. jr.
Date:
June 5, 1956
Publish Date ISO Format:
1956-06-05T00:00:00Z
Publication Start:
19560605
Publication End:
19560605
Corporate/Agency Author:
National Aeronautics and Space Administration
Publication month:
7
Publication year:
1956
Publication place:
Washington
SuDoc number:
Y 3.N 21/5:15/(letter-nos.)
Description:
cover title, 48+[6] p. il. 4°
Notes:
[No longer confidential. Classification changed May 29, 1959.] and (National Advisory Committee for Aeronautics.) [Processed.]
Notes:
(National Advisory Committee for Aeronautics.) [Processed.] † Distribution Made by Issuing Office.