Design and Thrust Analysis of Compact Jet Engine

Abstract

With gas turbine engine testing becoming very expensive because of the increasing complexity involved with the engine, engine subsystems, and test support systems, a low-cost Turbo Jet Engine is proposed. In the present study, The Turbo jet engine should built with modularity as a key design consideration to allow for flame-tube patterns and augmented sections to be changed quickly for combustion. Experiments that have gained impetus due to combustion anomalies/instabilities inherent with future military engine augmentors. This model allows for an effective way to test new analytical techniques before full scale testing at low-cost and quick schedule turnaround. The compact model should complete using a minor financial investment when matched to comparable capabilities.