NACA research memorandum RM (series). (National Advisory Committee for Aeronautics.) [Processed. No longer confidential.]. E56L06. Experimental investigation of 0.4 hub-tip diameter ratio axial-flow compressor inlet stage at transonic inlet relative Mach numbers: 4, Performance of tapered-tip rotor configuration with reset blade angles [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: 4, Performance of tapered-tip rotor configuration with reset blade angles [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.]. E56L06. Experimental investigation of 0.4 hub-tip diameter ratio axial-flow compressor inlet stage at transonic inlet relative Mach numbers: 4, Performance of tapered-tip rotor configuration with reset blade angles [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:
Washington, Feb. 28, 1957
Publish Date ISO Format:
1957-02-28T00:00:00Z
Publication Start:
19570228
Publication End:
19570228
Corporate/Agency Author:
National Aeronautics and Space Administration
Publication month:
11
Publication year:
1957
SuDoc number:
Y 3.N 21/5:15/(letter-nos.)
Description:
cover title, 34+ [4] p. il. 4°
Notes:
[Classification changed July 28, 1960.]
Notes:
[Classification changed July 28, 1960.] † Distribution Made by Issuing Office.