Technical notes. 2941. Drag of finite-length cylinders determined from flight tests at high Reynolds numbers for a Mach number range from 0.5 to 1.3 [with list of references]; by Clement J. Welsh.
Publication Title:
Drag of finite-length cylinders determined from flight tests at high Reynolds numbers for a Mach number range from 0.5 to 1.3 [with list of references]; by Clement J. Welsh.
Display Title:
Technical notes. 2941. Drag of finite-length cylinders determined from flight tests at high Reynolds numbers for a Mach number range from 0.5 to 1.3 [with list of references]; 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:
June 1953
Publish Date ISO Format:
1953-06-01T00:00:00Z
Publication Start:
19530601
Publication End:
19530630
Corporate/Agency Author:
National Advisory Committee for Aeronautics
Publication month:
7
Publication year:
1953
Publication place:
Washington
SuDoc number:
Y 3.N 21/5:6 (nos.)
Description:
cover title, 12 p.+[2] leaves, il. 4°
Notes:
[The 2 leaves in the collation consist of detachable catalog entries on heavy paper designed to be used in a card catalog.] and [Processed.]
Notes:
[Processed.] † Distribution Made by Issuing Office.