Effect of Exit Pressure Pulsation on the Performance and Stability Limit of a Turbocharger Centrifugal Compressor
Year: 2016
Type: article
DOI: 10.1115/1.4034689
Language: English
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
Funder: Imperial College London
OpenAlex ID: W4248919670
