Closure to “Discussion of ‘The Influence of Shrouded Stator Cavity Flows on Multistage Compressor Performance’” (1999, ASME J. Turbomach., 121, p. 497)
Year: 1999
Type: article
Abstract: We thank Ruixian Cai for his thoughtful discussion of our paper.We also appreciate the data he presented from an 11stage compressor, which show a significant change in performance due to the incorporation of shrouded vanes in place of cantilevered vanes.We are sure that others would not be so
Source: Journal of Turbomachinery
DOI: 10.1115/1.2841343
Authors: S. R. Wellborn, T. H. Okiishi
Institutions: Rolls-Royce (United States), Iowa State University
Language: English
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: bronze
OpenAlex ID: W2000711201