dc.contributor.other | Turbomachinery Symposium (42nd : 2013) | |
dc.creator | Sorokes, James M. | |
dc.date.accessioned | 2017-10-04T19:33:55Z | |
dc.date.available | 2017-10-04T19:33:55Z | |
dc.date.issued | 2013 | |
dc.identifier.uri | https://hdl.handle.net/1969.1/162913 | |
dc.description | Tutorial | en |
dc.description.abstract | The paper addresses the balance between peak attainable efficiency and overall operating range that must be addressed when specifying, designing and/or selecting centrifugal compressors. The relative roles of the various compressor components; i.e., impellers, diffusers, guide vanes, and return channels; in achieving the proper balance are discussed. Finally, the importance of proper component and stage aerodynamic matching is emphasized. | en |
dc.format.medium | Electronic | en |
dc.format.mimetype | application/pdf | |
dc.language.iso | en | |
dc.publisher | Texas A&M University. Turbomachinery Laboratories | |
dc.relation.ispartof | Proceedings of the 42nd Turbomachinery Symposium | en |
dc.subject.lcsh | Turbomachines | en |
dc.title | Range Versus Efficiency - Striking the Proper Balance | en |
dc.type.genre | Presentation | en |
dc.type.material | Text | en |
dc.identifier.doi | https://doi.org/10.21423/R1BP89 | |