Cold-air Performance of a 12.766-centimeter-tip-diameter Axial-flow Cooled Turbine


Book Description

A solid blade version of a single-stage, axial-flow turbine was investigated to determine its performance over a range of speeds from 0 to 105 percent of equivalent design speed and over a range of total to static pressure ratios from 1.62 to 5.07.
















NASA Technical Paper


Book Description




NASA Technical Paper


Book Description