Performance of Turbo Jet Engines Under the Influence of Supersonic Flight Disturbances(Leistungsverhalten von turbostrahltriebwerken unter dem einfluss von hyperschallflug-typischen eintrittsstroerungen)

摘要

This engineering dissertation investigates the impact of typical supersonic intake disturbances on the performance of a turbojet engine. Wind tunnel experiments are used to calculate the effects of Mach numbers and Reynold's numbers on a model-sized subsonic diffuser. A simulator is used to find ways to improve the performance of a turbo jet engine under supersonic conditions.