Effects of Local Mixing Ratios and Mass Flow Rates on Combustion Performance of the Fuel-Rich LOX (Liquid Oxygen)/kerosene Gas Generator in the ATR (Air Turbo Rocket) Engine

Effects of Local Mixing Ratios and Mass Flow Rates on Combustion Performance of the Fuel-Rich LOX (Liquid Oxygen)/kerosene Gas Generator in the ATR (Air Turbo Rocket) Engine

This paper presents a numerical simulation analysis of the flow and combustion characteristics of a fuel-rich LOX (liquid oxygen)/kerosene gas generator in an ATR (air turbo rocket) engine, examining the effects of local parameters on the combustion flow field and performance. The analysis considers...

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Bibliographic Details
Main Authors: Yuankun Zhang, Qingjun Zhao, Bin Hu, Qiang Shi, Wei Zhao, Xiaorong Xiang
Format: Article
Language:English
Published: MDPI AG 2023-06-01
Series:Aerospace
Subjects:
ATR engine
fuel-rich gas generator
bipropellant injector
unit injector mixing ratio
unit injector mass flow rate
combustion efficiency
Online Access:https://www.mdpi.com/2226-4310/10/6/545

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https://www.mdpi.com/2226-4310/10/6/545

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