The unsteady performance of a centrifugal compressor with different diffusers
- 1 January 2001
- journal article
- research article
- Published by SAGE Publications in Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy
- Vol. 215 (5), 585-599
- https://doi.org/10.1243/0957650011538820
Abstract
Unsteady flow in turbomachinery may be due to turbulence, wakes (rotor-stator interaction), inlet distortion, rotating stall or surge. It is undesired, because it may lead to narrow operation range, poor efficiency and blade failure due to vibration. Four low solidity vaned diffusers (LSVDs) together with one conventional vaned diffuser and two vaneless diffusers were tested downstream of the same impeller for the purpose of understanding the unsteady performance (stall and surge characteristics) of each diffuser and the performance relative to each other. This paper is a complementary paper to previous work where the design and overall and component performances of eight LSVDs have been reported.Keywords
This publication has 3 references indexed in Scilit:
- Application of a Low-Solidity Cascade Diffuser to Transonic Centrifugal CompressorJournal of Turbomachinery, 1990
- Experimental Study on Flow in a Supersonic Centrifugal ImpellerJournal of Engineering for Power, 1979
- Rotating Stall in a Radial Vaneless DiffuserJournal of Basic Engineering, 1964