Results 141 to 150 of about 33,160 (211)

A new model for compressor surge and stall control. [PDF]

open access: yesSci Rep
Shahriyari MJ   +3 more
europepmc   +1 more source

Characteristic variation of Mach number in subsonic co-flowing jets by varying lip thickness. [PDF]

open access: yesSci Rep
Kumar KS   +5 more
europepmc   +1 more source

Optimized efficiency axial-flow compressor

Applied Energy, 2005
A preliminary design efficiency-optimization of an axial-flow compressor, using one-dimensional flow theory, is studied in this paper. A model for the optimum design of a compressor stage, assuming a fixed distribution of axial velocities, is presented. The absolute inlet and exit angles of the rotor are taken as design variables.
Lingen Chen   +3 more
openaire   +3 more sources

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