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Foreword by Sir Geoffrey de Havilland
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aerodynamic air flow air intake aircraft speed airscrew altitude annular auxiliary axial compressor axial-flow axial-flow compressor boundary layer control British burners cent centrifugal compressor climb combustion chamber components compression cooling cruising cylinder Derwent diameter discharge driving ducted fan effect efficiency Electric employed exhaust fighter flight flying wing Frank Whittle fuel consumption fuselage gas turbine gases Gloster Gloster Meteor Goblin Havilland heat Heinkel-Hirth high speed ignition impeller increased inlet installation jet engine jet pipe jet unit jet-propelled aircraft Junkers load lower Mach number machine maximum Meteor mounted Nene nozzle operation orifice output performance piston engine possible power plant power unit pressure produce propeller pump radial ratio rear reciprocating engine reduced reduction gear ring rocket Rolls-Royce Rolls-Royce Derwent rotating rotor shaft stage static thrust stator blades steam steel take-off temperature thermal turbine blades turbine unit turbine-airscrew turbine-jet unit valve vanes weight Whittle