Browse TRAIL Inventories

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

Investigation of Blade Failures in a J34, Eleven-Stage Axial-Flow Compressor

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 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


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