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- 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
- 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