Lift (aircraft.) Effect of Mach and Reynolds numbers on maximum lift coefficient obtainable in gradual and abrupt stalls of pursuit airplane equipped with low-drag wing [with list of references]; by John R. Spreiter, George M. Galster, and William K. Blair.
Publication Title:
Lift (aircraft.) Effect of Mach and Reynolds numbers on maximum lift coefficient obtainable in gradual and abrupt stalls of pursuit airplane equipped with low-drag wing [with list of references]; by John R. Spreiter, George M. Galster, and William K. Blair.
Display Title:
Lift (aircraft.) Effect of Mach and Reynolds numbers on maximum lift coefficient obtainable in gradual and abrupt stalls of pursuit airplane equipped with low-drag wing [with list of references]; by John R. Spreiter, George M. Galster, and William K. Blair.
Corporate Agency Authors:
National Advisory Committee for Aeronautics
Sort Author:
National Advisory Committee for Aeronautics
Authors:
Spreiter, John R., Galster, George M., and Blair, William K.
Date:
[1947.]
Publish Date ISO Format:
1947-01-01T00:00:00Z
Publication Start:
19470101
Publication End:
19471231
Corporate/Agency Author:
National Advisory Committee for Aeronautics
Publication month:
13
Publication year:
1947
SuDoc number:
Y 3.N 21/5:11/A-5
Description:
cover title, 12 p. 16 pl. 4°
Notes:
(Wartime report A-5.) [Processed. Originally issued July 1945 as Memorandum report A5G06.]
Notes:
(Wartime report A-5.) [Processed. Originally issued July 1945 as Memorandum report A5G06.] † Distribution Made by Issuing Office.