Browse TRAIL Inventories

Efficiency tests of a single-stage impulse turbine having an 11.0-inch pitch-line diameter wheel with air as the driving fluid

The Performance of a Single-Stage Impulse Turbine Having an 11.0-Inch Pitch-Line Diameter Wheel with Cast Airfoil-Shaped and Bent Sheet-Metal Nozzle Blades

The effect of two inlet-duct designs on turbine efficiency

The Effect of Inlet Pressure and Temperature on the Efficiency of a Single Stage Impulse Turbine Having an 11.0-Inch Pitch-Line Diameter Wheel

Experimental investigation of performance and operating characteristics of a tail-pipe burner for a turbojet engine

Analytical and experimental investigation of thrust augmentation of axial- and centrifugal-compressor turbojet engines by injection of water and alcohol in combustion chambers

Experimental Study of Isothermal Wake-Flow Characteristics of Various Flame-Holder Shapes

Analysis of the turbojet engine for propulsion of supersonic fighter airplanes

A survey of methods for turbojet thrust measurement applicable to flight installation

Summary of NACA research on afterburners for turbojet engines


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