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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
- Altitude performance of annular combustor type turbojet engine with JFC-2 fuel
- Thrust augmentation of a turbojet engine by the introduction of liquid ammonia into the compressor inlet
- 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
- Combined compressor coolant injection and afterburning for turbojet thrust augmentation
- Influence of combustion-chamber length on afterburner performance
- 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
- Altitude performance of a full-scale turbojet engine using pentaborane fuels
- Influence of boric oxide deposition on turbojet-engine operation
- A study of temperature transients at the inlet of a turbojet engine
- Influence of Boric Oxide Deposition on Turbojet-Engine Operation