Potential increases in ideal stage pressure ratio theoretically possible in axial compressors; paper shows various configurations of flow diagram, for four individual cases, which result in considerable increases in ideal stage pressure ratio; considerations limited to ideal adiabatic flow through curved lattice types of blading.
High-speed flow through cambered rotating grids
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 15 , n 4
1948
5 pages
Aufsatz (Zeitschrift)
Englisch
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