Search U.S. government technical reports digitized or harvested by TRAIL.
Investigation of an impulse axial-flow compressor rotor over a range of blade angles
Application of the wire-mesh plotting device to incompressible cascade flows
Comparison of NACA 65-series compressor-blade pressure distributions and performance in a rotor and in cascade
The design and cascade tests of free-streamline and full-contour 160 degrees turning supersonic-turbine-blade sections
The Design and Cascade Tests of Free-Streamline and Full-Contour 160 Degree Turning Supersonic-Turbine-Blade Sections
Design and Investigation of a Transonic Axial-Flow Compressor Rotor With an Inlet Hub-Tip Radius Ratio of Essentially Zero