Dynamic and Nonlinear Simulation of Liquid-Propellant Engines

Author:

Karimi H.1,Nassirharand A.2,Beheshti M.3

Affiliation:

1. Khaje Nassir-Al-Deen Toosi University of Technology, 16579 Tehran, Iran

2. Farab Company, 15946 Tehran, Iran

3. University of Tehran, 14174 Tehran, Iran

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Cited by 21 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Transient Mathematical Modeling and Simulation for an Open Cycle Liquid Rocket Engine;Lecture Notes in Electrical Engineering;2022-09-30

2. Turbine inlet temperature effects on the start process of an expansion cycle liquid propellant rocket engine;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2022-06-14

3. Multivariable Control Coupling Analysis and ALQR Thrust Controller Design of Liquid Rocket Engine;2021 12th International Conference on Mechanical and Aerospace Engineering (ICMAE);2021-07-16

4. Dynamic Response of a Dual-Manifold Injector Rocket Engine to Throttling;Journal of Propulsion and Power;2018-11

5. Transient simulation of a differential piston warm gas self-pressurization system for liquid attitude and divert propulsion system;Chinese Journal of Aeronautics;2018-04

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