Usually the development of a new engine is initialized by the request of an aircraft manufacturer who formulates basic requirements for the propulsion system. Preliminary engine design is then the first design phase at the aero-engine manufacturer where the engineer’s task is to develop a proper engine concept fulfilling all requirements and to respond to the aircraft company in a short time. At this early design stage only simple models can be used, but the decisions made are far-reaching and need to be precise. Therefore, engine component scaling tools are applied to increase prediction accuracy.
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