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AIRCRAFT GAS TURBINES with CENTRIFUGAL COMPRESSORS

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Hall, R. S., author.
Conference Name:
SAE National Aeronautic Meeting
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1946
Summary:
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
Notes:
Vendor supplied data
Publisher Number:
460239
Access Restriction:
Restricted for use by site license

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