Technical notes. 2649. Effect of Mach number on flow and application of compressibility corrections in 2-dimensionnl subsonic-transsonic compressor cascade having varied porous-wall suction at blade tins [with list of references]; by William B. Briggs.
Publication Title:
Effect of Mach number on flow and application of compressibility corrections in 2-dimensionnl subsonic-transsonic compressor cascade having varied porous-wall suction at blade tins [with list of references]; by William B. Briggs.
Display Title:
Technical notes. 2649. Effect of Mach number on flow and application of compressibility corrections in 2-dimensionnl subsonic-transsonic compressor cascade having varied porous-wall suction at blade tins [with list of references]; by William B. Briggs.
Series Title:
Technical notes.
Corporate Agency Authors:
National Advisory Committee for Aeronautics
Sort Author:
National Advisory Committee for Aeronautics
Authors:
Briggs, William B.
Date:
Mar. 1952
Publish Date ISO Format:
1952-03-01T00:00:00Z
Publication Start:
19520301
Publication End:
19520331
Corporate/Agency Author:
National Advisory Committee for Aeronautics
Publication month:
10
Publication year:
1952
Publication place:
Washington
SuDoc number:
Y 3.N 21/5:6/(nos.)
Description:
cover title, 43+[6] p. il. 4°
Notes:
[Processed.]
Notes:
[Processed.] † Distribution Made by Issuing Office.