Comparative Analysis of a High Bypass Turbofan using a Pulsed Detonation Combustor
Ionio Q. Q. Andrus
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Comparative Analysis of a High Bypass Turbofan using a Pulsed Detonation Combustor

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It has been proposed that the implementation of a pulsed detonation combustor in a high-bypass turbofan engine would result in an engine that is both more efficient and more reliable. The validity of the performance claims are evaluated based on a comparison between the baseline and hybrid turbofans as modeled in the Numerical Propulsion System Simulation (NPSS). The engine cycle of the baseline high-bypass turbofan is evaluated and compared using both the Aircraft Engine Design System (AEDsys) and NPSS programs. The baseline engine agreed to within 1% on the net thrust calculation and specifi...