Browse TRAIL Inventories

Altitude investigation of three flame-holder and fuel-systems configurations in a short converging afterburner on a turbojet engine

Comparison of Turbojet-Engine Altitude Performance Characteristics and Ignition Limits With MIL-F-5624A Fuel, Grades JP-3 and JP-4

Component and over-all performance evaluation of a J47-GE-25 turbojet engine over a range of engine-inlet Reynolds number indices

Altitude evaluation of several afterburner design variables on a J47-GE-17 turbojet engine

Influence of combustion-chamber length on afterburner performance

Influence of Combustion-chamber Length on Afterburner Performance

Rotating-Stall and Rotor-Blade-Vibration Survey of a 13-Stage Axial-Flow Compressor in a Turbojet Engine

Turbine Failure Investigation of J65-W-4 Turbojet Engine in an Altitude Test Chamber

Design and performance of flight-type liquid-hydrogen heat exchanger

Altitude chamber evaluation of an aircraft liquid hydrogen fuel system used with a turbojet engine

Design and performance of flight-type liquid-hydrogen heat exchanger


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