Technical notes. 3172. Effects of leading-edge radius and maximum thickness-chord ratio on variation with Mach number of aerodynamic characteristics of several thin NACA airfoil sections [with list of references]; by Robert E. Berggren and Donald J. Graham.
Publication Title:
Effects of leading-edge radius and maximum thickness-chord ratio on variation with Mach number of aerodynamic characteristics of several thin NACA airfoil sections [with list of references]; by Robert E. Berggren and Donald J. Graham.
Display Title:
Technical notes. 3172. Effects of leading-edge radius and maximum thickness-chord ratio on variation with Mach number of aerodynamic characteristics of several thin NACA airfoil sections [with list of references]; by Robert E. Berggren and Donald J. Graham.
Series Title:
Technical notes.
Corporate Agency Authors:
National Advisory Committee for Aeronautics
Sort Author:
National Advisory Committee for Aeronautics
Authors:
Berggren, Robert E. and Graham, Donald J.
Date:
Apr. 14, 1954
Publish Date ISO Format:
1954-04-14T00:00:00Z
Publication Start:
19540414
Publication End:
19540414
Corporate/Agency Author:
National Advisory Committee for Aeronautics
Publication month:
9
Publication year:
1954
Publication place:
Washington
SuDoc number:
Y 3.N 21/5:6/(nos.)
Description:
cover title, 65 p.+ [2] leaves, il. 4°
Notes:
[Supersedes NACA RM A50D04, 1950.] and [Processed. The pages or leaves in brackets in each collation consist of detachable card catalog entries.]
Notes:
[Processed. The pages or leaves in brackets in each collation consist of detachable card catalog entries.] † Distribution Made by Issuing Office.