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- Elimination of Galling of Pendulum-Vibration Dampers Used in Aircraft Engines
- Vibration Survey of Blades in 19XB Axial-Flow Compressor 2: Dynamic Investigation
- Vibration Survey of Blades in 19XB Axial-Flow Compressor 3: Preliminary Engine Investigation
- Vibration Survey of NACA 24-Inch Supersonic Axial-Flow Compressor
- Vibration Survey of Blades in 10-Stage Axial-Flow Compressor 1: Static Investigation
- Effects of Obstructions in Compressor Inlet on Blade Vibration in 10-Stage Axial-Flow Compressor
- Effect of Angle of Incidence of Second-Stage Vane Assembly on Third-Stage Compressor-Blade Vibration and Engine Performance
- Preliminary Investigation in J33 Turbojet Engine of Several Root Designs for Ceramal Turbine Blades
- The Design of Brittle-Material Blade Roots Based on Theory and Rupture Tests of Plastic Models
- Comparative Tensile Strengths at 1200 Degrees F of Various Root Designs for Cermet Turbine Blades
- Investigation of Blade Failures in a J34, Eleven-Stage Axial-Flow Compressor
- Investigation of Mechanical Fastenings for Solid Turbine Blades Made From Ductile Materials
- Correlation of Vibratory Root Failures and Stress Distribution in J65 Compressor Blades
- The Design of Brittle-Material Blade Roots Based on Theory and Rupture Tests of Plastic Models
- Structural Design and Engine Evaluation of an Air-Cooled Turbine Blade Composed of Corrugation and a Semistrut for Operation at a Tip Speed of 1200 Feet Per Second
- Design and Engine Evaluation of a Semistrut Corrugated Air-Cooled Turbine Blade for Operation at a Tip Speed of 1300 Feet Per Second