Some Advantages and Limitations of CENTRIFUGAL and AXIAL AIRCRAFT COMPRESSORS

450224

01/01/1945

Event
Pre-1964 SAE Technical Papers
Authors Abstract
Content
IN understanding this investigation on centrifugal and axial compressors, the authors point out, it must be remembered that the centrifugal compressor has enjoyed years of intensive development because of its use as a supercharger, while the axial compressor has been denied such attention until recently.
It is also explained that performance and space-weight considerations must be well balanced for a supercharger used on reciprocating engines, while with nonreciprocating engines, by far the most important compressor consideration is optimum performance.
The conclusion of the authors is that the axial compressor will ultimately probably be used in applications where compressor efficiency above 80% is at a high premium, but this can happen only after it has been brought into line from the standpoint of operating range and light structural design combined with ruggedness.
Meta TagsDetails
DOI
https://doi.org/10.4271/450224
Pages
14
Citation
CAMPBELL, K., and TALBERT, J., "Some Advantages and Limitations of CENTRIFUGAL and AXIAL AIRCRAFT COMPRESSORS," SAE Technical Paper 450224, 1945, https://doi.org/10.4271/450224.
Additional Details
Publisher
Published
Jan 1, 1945
Product Code
450224
Content Type
Technical Paper
Language
English