Numerical Simulation of Hybrid Rockets Liquid Injection and Comparison with Experiments-Reference-Cited by-同舟云学术

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Numerical Simulation of Hybrid Rockets Liquid Injection and Comparison with Experiments

Published:2015-01 Issue:1 Volume:31 Page:352-364
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Lazzarin M.¹,Faenza M.¹,Barato F.¹,Bellomo N.¹,Bettella A.¹

Affiliation:

1. Department of Industrial Engineering (DII), University of Padua, 35131 Padua, Italy

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

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

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.B35223

Reference20 articles.

1. Navier-Stokes Investigation on Reacting Flow Field of HTPB/O2 Hybrid Motor and Regression Rate Evaluation

2. A Physics Based Comprehensive Mathematical Model to Predict Motor Performance in Hybrid Rocket Propulsion Systems

3. Simulation Code for Hybrid Rocket Combustion

4. 2D transient numerical code for hybrid rocket simulations with detailed chemistry

Cited by 7 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. Modeling and CFD Simulation of Regression Rate in Hybrid Rocket Motors;Fire;2023-03-02

2. Experimental Investigation of Throttleable H2O2 and Polypropylene Hybrid Rocket Motor;Journal of Propulsion and Power;2023-01

3. CFD simulations of a N2O/paraffin fueled hybrid rocket to perform capture maneuvers in a Mars orbit;AIAA Propulsion and Energy 2021 Forum;2021-07-28

4. Explicit Analytical Equations for Single Port Hybrid Rocket Combustion Chamber Sizing;Journal of Propulsion and Power;2020-11

5. Development of a Flow Control Valve for a Throttleable Hybrid Rocket Motor and Throttling Fire Tests;2018 Joint Propulsion Conference;2018-07-08

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