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Experimental investigation of thrust augmentation of 4000-pound-thrust axial-flow-type turbojet engine by interstage injection of water-alcohol mixtures in compressor

Experimental investigation of turbojet-engine thrust augmentation by combined compressor coolant injection and tail-pipe burning

Thrust Augmentation of a Turbojet Engine at Simulated Flight Conditions by Introduction of a Water-Alcohol Mixture into the Compressor

Thrust augmentation of a turbojet engine by the introduction of liquid ammonia into the compressor inlet

Altitude performance of annular combustor type turbojet engine with JFC-2 fuel

Turbojet-engine thrust augmentation at altitude by combined ammonia injection into the compressor inlet and afterburning

Combined Compressor Coolant Injection and Afterburning for Turbojet Thrust Augmentation

Preliminary Altitude Performance Data of J71-A2 Turbojet Engine Afterburner

Preliminary Altitude Performance Data for the J71-A2 (X-26) Turbojet Engine

Influence of combustion-chamber length on afterburner performance

Combined compressor coolant injection and afterburning for turbojet thrust augmentation

Influence of Combustion-chamber Length on Afterburner Performance

Altitude Performance of Modified J71 Afterburner with Revised Engine Operating Conditions

Altitude performance evaluation of J71-A-11 turbojet engine

Extended operation of turbojet engine with pentaborane

Influence of boric oxide deposition on turbojet-engine operation

A study of temperature transients at the inlet of a turbojet engine

Altitude performance of a full-scale turbojet engine using pentaborane fuels

Influence of Boric Oxide Deposition on Turbojet-Engine Operation


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