NACA research memorandum RM (series). (National Advisory Committee for Aeronautics.) [Processed. No longer confidential.]. E55L09. Experimental investigation of 0.4 hub tip diameter ratio axial-flow compressor inlet stage at transonic inlet relative Mach numbers: 3, Effect of tip taper on over-all and blade-element performances [with list of references]: by John C. Montgomery and Frederick Glaser.
Publication Title:
Experimental investigation of 0.4 hub tip diameter ratio axial-flow compressor inlet stage at transonic inlet relative Mach numbers: 3, Effect of tip taper on over-all and blade-element performances [with list of references]: by John C. Montgomery and Frederick Glaser.
Display Title:
NACA research memorandum RM (series). (National Advisory Committee for Aeronautics.) [Processed. No longer confidential.]. E55L09. Experimental investigation of 0.4 hub tip diameter ratio axial-flow compressor inlet stage at transonic inlet relative Mach numbers: 3, Effect of tip taper on over-all and blade-element performances [with list of references]: by John C. Montgomery and Frederick Glaser.
Series Title:
NACA research memorandum RM (series). (National Advisory Committee for Aeronautics.) [Processed. No longer confidential.]
Corporate Agency Authors:
National Aeronautics and Space Administration
Sort Author:
National Aeronautics and Space Administration
Authors:
Montgomery, John C. and Glaser, Frederick
Date:
Mar. 30, 1956
Publish Date ISO Format:
1956-03-30T00:00:00Z
Publication Start:
19560330
Publication End:
19560330
Corporate/Agency Author:
National Aeronautics and Space Administration
Publication month:
10
Publication year:
1956
Publication place:
Washington
SuDoc number:
Y 3.N 21/5:15/(letter-nos.)
Description:
cover title, 35 p. + 2 leaves, il. 4°
Notes:
[Classification changed July 28, 1960.]
Notes:
[Classification changed July 28, 1960.] † Distribution Made by Issuing Office.