Development and Validation of a 1.5-D Combustion Chamber Model for a Hybrid Rocket Engine Applied to a Cylindrical HDPE Chamber-Reference-Cited by-同舟云学术

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Development and Validation of a 1.5-D Combustion Chamber Model for a Hybrid Rocket Engine Applied to a Cylindrical HDPE Chamber

Published:2021-07-28 Issue: Volume: Page:
ISSN:
Container-title:AIAA Propulsion and Energy 2021 Forum
language:
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Author:

Quero Granado Elena¹,Hijlkema Jouke¹,Lestrade Jean-Yves¹,Anthoine Jerome¹

Affiliation:

1. ONERA

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2021-3495

Reference61 articles.

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

2. Transient Computational Thermofluid-Dynamic Simulation of Hybrid Rocket Internal Ballistics

3. Mazzetti, A. “Numerical Modeling and Simulations of Combustion Processes in Hybrid Rocket Engines,” Ph.D. thesis, Politecnico di Milano,Mathematics Department F. Brioschi, Feb. 2014.

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