Technical notes. 2828. Effect of finite trailing-edge thickness on drag of rectangular and delta wings at supersonic speeds [with list of references]; by E. B. Klunker and Conrad Rennemann, jr.
Publication Title:
Effect of finite trailing-edge thickness on drag of rectangular and delta wings at supersonic speeds [with list of references]; by E. B. Klunker and Conrad Rennemann, jr.
Display Title:
Technical notes. 2828. Effect of finite trailing-edge thickness on drag of rectangular and delta wings at supersonic speeds [with list of references]; by E. B. Klunker and Conrad Rennemann, jr.
Series Title:
Technical notes.
Corporate Agency Authors:
National Advisory Committee for Aeronautics
Sort Author:
National Advisory Committee for Aeronautics
Authors:
Klunker, E. B. and Rennemann, Conrad jr.
Date:
Nov. 1952
Publish Date ISO Format:
1952-11-01T00:00:00Z
Publication Start:
19521101
Publication End:
19521130
Corporate/Agency Author:
National Advisory Committee for Aeronautics
Publication month:
2
Publication year:
1952
Publication place:
Washington
SuDoc number:
Y 3.N 21/5:6/(nos.)
Description:
cover title, 26+ [2] p. il. 4°
Notes:
[Processed.]
Notes:
[Processed.] † Distribution Made by Issuing Office.