Continuation of studies initiated in 1944 regarding potential improvements of turbojet propulsion systems for supersonic flight; comparison of some aspects of axial compressor design for accommodating high rate of mass flow.
Simplified design comparisons of axial compressors
J. Aeronautical Sciences
Journal of the Aeronautical Sciences ; 18 , n 7
1951
13 pages
Aufsatz (Zeitschrift)
Englisch
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