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Performance of NACA Eight-stage Axial-flow Compressor Designed on the Basis of Airfoil Theory
John T. Sinnette
Oscar W. Schey
J. Austin King
出版
National Advisory Committee for Aeronautics
, 1944
URL
http://books.google.com.hk/books?id=dm_1G84ED_IC&hl=&source=gbs_api
EBook
FULL_PUBLIC_DOMAIN
註釋
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.
