Since the inception of the first gas turbine engines, scientists and aircraft propulsion designers have attempted to improve engine efficiency, size, weight, fuel consumption and power output. In the current scenario, where ...

This thesis constitutes the first research project into reverse thrust aerodynamics of variable-pitch turbofans within the Cranfield Rolls-Royce UTC in Aero System Design, Integration & Performance. The study focussed on ...

The effective and efficient evaluation of conceptual product designs prior to manufacturing of prototypes, is of utmost importance for any industrial ac¬tivity. The rotorcraft industry is no different. Accurate, thorough ...

Current developments of civil and military applications may require the installation of aero-engines embedded into the aircraft structure. Consequently, complex diffusing Sducts are necessary to convey air from the intake ...