Author : John T. Sinnette,Oscar W. Schey,J. Austin King
Publisher : Unknown
Page : 74 pages
File Size : 53,5 Mb
Release : 1944
Category : Aerofoils
ISBN : UOM:39015095014299
Performance of NACA Eight-stage Axial-flow Compressor Designed on the Basis of Airfoil Theory by John T. Sinnette,Oscar W. Schey,J. Austin King Pdf
The NACA has conducted an investigation to determine the performance that can be obtained from a multistage axial-flow compressor based on airfoil research. A theory was developed; an eight-stage axial-flow compressor was designed, constructed, and tested.