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Flugtriebwerk
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Three-Dimensional Inverse Design Method for Turbine and Compressor Blades
The value of early flight evaluation of propulsion concepts using the NASA F-15 research airplane
The United Kingdom engine technology demonstrator programme
The supersonic through-flow turbofan for high Mach propulsion
The supersonic through-flow turbofan for high Mach propulsion
The supersonic fan engine: An advanced concept in supersonic cruise propulsion
The spark-ignition aircraft piston engine of the future
The simulation of aircraft engine oil deposits under static conditions and their influencing factors
The selection of materials technologies for full-scale development
The selection of convertible engines with current gas generator technology for high speed rotorcraft
The selection of convertible engines with current gas generator technology for high speed rotorcraft
The science, technology, and implementation of TiAl alloys in commercial aircraft engines
The Rolls-Royce civil engine family - Today and into the future
The role of PM in the design of lightweight aircraft engine components
The Role of Modern Control Theory in the Design of Controls for Aircraft Turbine Engines
THE REDUCTION OF CHEMICAL KINETIC MECHANISMS IN HIGH-TEMPERATURE HETEROGENEOUS FLOWS IN A NOZZLE
The PW100 Engine: 20 Years of Gas Turbine Technology Evolution
The Potential of Advanced Materials on Structural Design of Future Aircraft Engines
Theory for the Use of Foreign Gas in Simulating Film Cooling
The oil/air system of a modern fighter aircraft engine