The design philosophy and development of three recent Rolls-Royce centrifugal compressors, ranging in pressure ratio from 3.6 to 7, are described. The main geometrical and aerodynamic details are given, together with overall performance characteristics of the compressors.
Recent Experience on Centrifugal Compressors for Small Gas Turbines
- Views Icon Views
- Share Icon Share
- Search Site
Beard, MG, Pratt, CM, & Timmis, PH. "Recent Experience on Centrifugal Compressors for Small Gas Turbines." Proceedings of the ASME 1978 International Gas Turbine Conference and Products Show. Volume 1B: General. London, England. April 9–13, 1978. V01BT02A091. ASME. https://doi.org/10.1115/78-GT-193
Download citation file: