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AIRCRAFT GAS TURBINES with CENTRIFUGAL COMPRESSORS
ISSN: 0148-7191, e-ISSN: 2688-3627
Published January 01, 1946 by SAE International in United States
Annotation ability available
ALONG with further improvements in the form of increased flow and pressure ratio for gas turbines with centrifugal compressors, the author looks forward to an improvement in efficiency, this latter factor being more important in gas turbines than in aircraft turbosuperchargers.
As an aid to the realization of this aim, the author presents here a method of determining approximate gas turbine performance at various operating conditions.