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- Summary of Investigations of Mark 25 Aerial-Torpedo Turbine
- Effect of Certain Combinations of Wall Contouring and Design Exit Velocity Distribution on Prediction of Turbine-Nozzle Mass Flow
- Investigation of Turbines for Driving Supersonic Compressors 5: Design and Performance of Third Configuration With Nontwisted Rotor Blades
- Investigation of Turbines for Driving Supersonic Compressors 3: First Configuration With Four Nozzle Settings and One Nozzle Modification
- Investigation of Turbines for Driving Supersonic Compressors 4: Design and Performance of Second Configuration Including Study of Three-Dimensional Flow Effects
- Analytical investigation of off-design performance of a transonic turbine
- Effect of Nozzle Secondary Flows on Turbine Performance as Indicated by Exit Surveys of a Rotor
- Investigation of a Transonic Turbine Designed for a Maximum Rotor-Blade Suction-Surface Relative Mach Number of 1.57
- Effect of Reduced Stator-Blade Trailing-Edge Thickness on Over-All Performance of a Transonic Turbine
- Use of effective momentum thickness in describing turbine rotor-blade losses
- Experimental Investigation of Turbine Stator-Blade-Outlet Boundary-Layer Characteristics and a Comparison With Theoretical Results
- Tabulation of Mass-Flow Parameters for Use in Design of Turbomachine Blade Rows for Ratios of Specific Heats of 1.3 and 1.4
- Experimental Investigation of a 7-Inch-Tip-Diameter Transonic Turbine
- Experimental Investigation of a 7-Inch-Tip-Diameter Transonic Turbine