Pseudo-Two-Dimensional Modeling and Validation of a Hybrid Rocket Combustion Chamber-Reference-Cited by-同舟云学术

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Pseudo-Two-Dimensional Modeling and Validation of a Hybrid Rocket Combustion Chamber

Published:2022-11 Issue:6 Volume:38 Page:957-972
ISSN:1533-3876
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Quero Granado Elena¹,Hijlkema Jouke¹,Lestrade Jean-Yves¹,Anthoine Jérôme¹

Affiliation:

1. ONERA/DMPE, University of Toulouse, F-31055 Toulouse, France

Funder

ONERA

Centre National d'Etudes Spatiales

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

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

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.B38682

Reference65 articles.

1. Special Issue “Advances in Hybrid Rocket Technology and Related Analysis Methodologies”

2. Turbulence Modeling Effects on Fuel Regression Rate in Hybrid Rocket Numerical Simulations

3. New Entrainment Model for Modelling the Regression Rate in Hybrid Rocket Engines

Cited by 3 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. Effect of grain length on GOx-paraffin hybrid rocket engines performance and regression rate;International Journal of Heat and Mass Transfer;2024-03

2. Bridging the Technology Gap: Strategies for Hybrid Rocket Engines;Aerospace;2023-10-22

3. Combustion Characteristics of a Swirl-Radial-Injection Composite Fuel Grain with Applications in Hybrid Rockets;Aerospace;2023-08-28

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