NACA research memorandum RM (series). E55K23. Effect of inlet-gulde-vane angle on performance characteristics of 13-stage axial-flow compressor in turbojet engine [with list of references]; by Arthur A. Medeiros and Howard F. Calvert.
Publication Title:
Effect of inlet-gulde-vane angle on performance characteristics of 13-stage axial-flow compressor in turbojet engine [with list of references]; by Arthur A. Medeiros and Howard F. Calvert.
Display Title:
NACA research memorandum RM (series). E55K23. Effect of inlet-gulde-vane angle on performance characteristics of 13-stage axial-flow compressor in turbojet engine [with list of references]; by Arthur A. Medeiros and Howard F. Calvert.
Series Title:
NACA research memorandum RM (series).
Corporate Agency Authors:
National Aeronautics and Space Administration
Sort Author:
National Aeronautics and Space Administration
Authors:
Medeiros, Arthur A. and Calvert, Howard 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, 25 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.