Transonic investigation of an axial-flow compressor rotor with a hub-tip ratio of 0.75 and blades having NACA A(sub 2)I(Sub 8b) mean lines
Description: No Description Available.
Date: September 30, 1957
Creator: Bernot, Peter T & Savage, Melvyn
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department