A Comparative Performance Analysis of the Novel TurboAux Engine with a Turbojet Engine, and a Low-Bypass Ratio Turbofan Engine with an Afterburner

A Comparative Performance Analysis of the Novel TurboAux Engine with a Turbojet Engine, and a Low-Bypass Ratio Turbofan Engine with an Afterburner

Presented herein is a comparative performance analysis of a novel turbofan engine with an auxiliary combustion chamber, nicknamed the TurboAux engine, against a turbojet engine, and a low bypass ratio turbofan engine with an afterburner is presented. The TurboAux engine is an adaption of the low-byp...

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Bibliographic Details
Main Authors: Kaleab Fetahi, Sharanabasaweshwara A. Asundi, Arthur C. Taylor
Format: Article
Language:English
Published: MDPI AG 2022-10-01
Series:International Journal of Turbomachinery, Propulsion and Power
Subjects:
turbojet
turbofan
afterburner
optimization
auxiliary combustion
Online Access:https://www.mdpi.com/2504-186X/7/4/28

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