Technical notes. 3607. Effect of thickness, camber, and thickness distribution on airfoil characteristics at Mach numbers up to 1.0 [with list of references]; by Bernard N. Daley and Richard S. Dick.
Publication Title:
Effect of thickness, camber, and thickness distribution on airfoil characteristics at Mach numbers up to 1.0 [with list of references]; by Bernard N. Daley and Richard S. Dick.
Display Title:
Technical notes. 3607. Effect of thickness, camber, and thickness distribution on airfoil characteristics at Mach numbers up to 1.0 [with list of references]; by Bernard N. Daley and Richard S. Dick.
Series Title:
Technical notes.
Corporate Agency Authors:
National Advisory Committee for Aeronautics
Sort Author:
National Advisory Committee for Aeronautics
Authors:
Daley, Bernard N. and Dick, Richard S.
Date:
Mar. 1956
Publish Date ISO Format:
1956-03-01T00:00:00Z
Publication Start:
19560301
Publication End:
19560331
Corporate/Agency Author:
National Advisory Committee for Aeronautics
Publication month:
10
Publication year:
1956
Publication place:
Washington
SuDoc number:
Y 3.N 21/5:6/(nos.)
Description:
cover title, 75 p.+ [3] leaves, il. 4°
Notes:
[Supersedes declassified Research memorandum L52G31a, 1952.] 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.