Technical notes. 3650. Results of flight investigation to determine zero-lift drag characteristics of 60° delta wing with NACA 65-006 airfoil section and various doublewedge sections at Mach numbers from 0.7 to 1.6 [with one reference]; by Clement J. Welsh.
Publication Title:
Results of flight investigation to determine zero-lift drag characteristics of 60° delta wing with NACA 65-006 airfoil section and various doublewedge sections at Mach numbers from 0.7 to 1.6 [with one reference]; by Clement J. Welsh.
Display Title:
Technical notes. 3650. Results of flight investigation to determine zero-lift drag characteristics of 60° delta wing with NACA 65-006 airfoil section and various doublewedge sections at Mach numbers from 0.7 to 1.6 [with one reference]; by Clement J. Welsh.
Series Title:
Technical notes.
Corporate Agency Authors:
National Advisory Committee for Aeronautics
Sort Author:
National Advisory Committee for Aeronautics
Authors:
Welsh, Clement J.
Date:
Apr. 1956
Publish Date ISO Format:
1956-04-01T00:00:00Z
Publication Start:
19560401
Publication End:
19560430
Corporate/Agency Author:
National Advisory Committee for Aeronautics
Publication month:
9
Publication year:
1956
Publication place:
Washington
SuDoc number:
Y 3.N 21/5:6/(nos.)
Description:
cover title, 13 p.+[2] leaves, il. 4°
Notes:
[Supersedes declassified NACA Research memorandum L50F01, 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.