Static pressure. Effect of Mach number on position error as applied to pitotstatic tube located 0.55 chord ahead of airplane wing [with list of references]; by W. F. Lindsey.
Publication Title:
Static pressure. Effect of Mach number on position error as applied to pitotstatic tube located 0.55 chord ahead of airplane wing [with list of references]; by W. F. Lindsey.
Display Title:
Static pressure. Effect of Mach number on position error as applied to pitotstatic tube located 0.55 chord ahead of airplane wing [with list of references]; by W. F. Lindsey.
Corporate Agency Authors:
National Advisory Committee for Aeronautics
Sort Author:
National Advisory Committee for Aeronautics
Authors:
Lindsey, W. F.
Date:
[1946.]
Publish Date ISO Format:
1946-01-01T00:00:00Z
Publication Start:
19460101
Publication End:
19461231
Corporate/Agency Author:
National Advisory Committee for Aeronautics
Publication month:
13
Publication year:
1946
SuDoc number:
Y 3.N 21/5:11/L-75
Description:
cover title, 5 p. 5 pl. 4°
Notes:
(Wartime report L-75.) [Processed. Originally issued May 1944 as Confidential bulletin L4E29.]
Notes:
(Wartime report L-75.) [Processed. Originally issued May 1944 as Confidential bulletin L4E29.] † Distribution Made by Issuing Office.