AIRCRAFT GAS TURBINES with CENTRIFUGAL COMPRESSORS

460239

01/01/1946

Event
Pre-1964 SAE Technical Papers
Authors Abstract
Content
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.
Meta TagsDetails
DOI
https://doi.org/10.4271/460239
Pages
5
Citation
HALL, R., "AIRCRAFT GAS TURBINES with CENTRIFUGAL COMPRESSORS," SAE Technical Paper 460239, 1946, https://doi.org/10.4271/460239.
Additional Details
Publisher
Published
Jan 1, 1946
Product Code
460239
Content Type
Technical Paper
Language
English