Numerical simulation of ducted rocket motor-Reference-Cited by-同舟云学术

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Numerical simulation of ducted rocket motor

Published:2001-07-08 Issue: Volume: Page:
ISSN:
Container-title:37th Joint Propulsion Conference and Exhibit
language:
Short-container-title:

Author:

Ristori Arnaud¹,Dufour Emmanuel²

Affiliation:

1. ONERA, Palaiseau, France

2. EADS Aerospatiale Matra Missiles, Chatillon, France

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2001-3193

Cited by 14 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. CFD Driven Aero-Propulsive Design of a Ducted Ramjet Missile;Journal of Aerospace Sciences and Technologies;2023-07-29

2. Numerical Simulation of Reacting Flow Field in a Solid-Propellant Ducted Rocket;Energy and Exergy for Sustainable and Clean Environment, Volume 2;2022-09-19

3. Study on Combustion Flow-Field of Solid Ducted Rocket with Multiple Gas Nozzles;2021 12th International Conference on Mechanical and Aerospace Engineering (ICMAE);2021-07-16

4. An LES for the Effects of Particle Size and Velocity Ratio on the Flow Structure in the Secondary Combustor;International Journal of Aeronautical and Space Sciences;2020-07-20

5. Characteristics of the combustion chamber of a boron-based solid propellant ducted rocket with a chin-type inlet;Aerospace Science and Technology;2018-11

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