NACA research memorandum RM (series). E55K03. Effect of inlet-guide-vane angle on blade vibration and rotating stall of 13-stage axial-flow compressor in turbojet engine [with list of references]; by Howard F. Calvert, Arthur A. Medeiros, and Donald F. Johnson.
Publication Title:
Effect of inlet-guide-vane angle on blade vibration and rotating stall of 13-stage axial-flow compressor in turbojet engine [with list of references]; by Howard F. Calvert, Arthur A. Medeiros, and Donald F. Johnson.
Display Title:
NACA research memorandum RM (series). E55K03. Effect of inlet-guide-vane angle on blade vibration and rotating stall of 13-stage axial-flow compressor in turbojet engine [with list of references]; by Howard F. Calvert, Arthur A. Medeiros, and Donald F. Johnson.
Series Title:
NACA research memorandum RM (series).
Corporate Agency Authors:
National Aeronautics and Space Administration
Sort Author:
National Aeronautics and Space Administration
Authors:
Calvert, Howard F., Medeiros, Arthur A., and Johnson, Donald F.
Date:
May 22, 1956
Publish Date ISO Format:
1956-05-22T00:00:00Z
Publication Start:
19560522
Publication End:
19560522
Corporate/Agency Author:
National Aeronautics and Space Administration
Publication month:
8
Publication year:
1956
SuDoc number:
Y 3.N 21/5:15/(letter-nos.)
Description:
cover title, 21 p. +[2]. leaves, il. 4°
Notes:
(National Advisory Committee for Aeronautics.) [Processed. No longer confidential. Classification changed Apr. 12, 1961.]
Notes:
(National Advisory Committee for Aeronautics.) [Processed. No longer confidential. Classification changed Apr. 12, 1961.] † Distribution Made by Issuing Office.