Description: From Introduction: "This report presents data from measurements of the flow in a single-stage research compressor, which supports the model of reference 1. A calculated shock technique similar to that of reference 1 is incorporated with these experimental results. Another approach for estimating passage shock loss given a flow rate and blade geometry was reported in reference 2."
Date: June 5, 1958
Creator: Lewis, George W; Tysl, Edward R & Fessler, Theodore E
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department