NACA research memorandum RM (series). A57H19. Effects of leading-edge slat and trailing-edge split flap on aerodynamic characteristics of wing-fuselage combination having nearly triangular wing of aspect ratio 2.9 at Mach numbers from 0.60 to 0.92 [with list of references]; by Fred A. Demele.
Publication Title:
Effects of leading-edge slat and trailing-edge split flap on aerodynamic characteristics of wing-fuselage combination having nearly triangular wing of aspect ratio 2.9 at Mach numbers from 0.60 to 0.92 [with list of references]; by Fred A. Demele.
Display Title:
NACA research memorandum RM (series). A57H19. Effects of leading-edge slat and trailing-edge split flap on aerodynamic characteristics of wing-fuselage combination having nearly triangular wing of aspect ratio 2.9 at Mach numbers from 0.60 to 0.92 [with list of references]; by Fred A. Demele.
Series Title:
NACA research memorandum RM (series).
Corporate Agency Authors:
National Aeronautics and Space Administration
Sort Author:
National Aeronautics and Space Administration
Authors:
Demele, Fred A.
Date:
Washington, Jan. 24, 1958
Publish Date ISO Format:
1958-01-24T00:00:00Z
Publication Start:
19580124
Publication End:
19580124
Corporate/Agency Author:
National Aeronautics and Space Administration
Publication month:
12
Publication year:
1958
SuDoc number:
Y 3.N 21/5:15/(letter-nos.)
Description:
cover title, 66 p.+[2] leaves, 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.