Performance Prediction of a Ducted Rocket Combustor Using a Simulated Solid Fuel-Reference-Cited by-同舟云学术

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Performance Prediction of a Ducted Rocket Combustor Using a Simulated Solid Fuel

Published:2004-09 Issue:5 Volume:20 Page:936-944
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Stowe Robert A.,Dubois Charles,Harris Paul G.,Mayer Alfons E.H.J.¹,deChamplain Alain,Ringuette Sophie

Affiliation:

1. TNO Prins Maurits Laboratory, 2280 AA Rijswijk, The Netherlands

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/10.2514/1.2799

Reference43 articles.

Cited by 26 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. Stochastic Equilibrium Analysis to Optimize Solid Propellant Combustion Gas Composition;Journal of Propulsion and Power;2024-09

2. Performance Analysis of a Ducted Rocket Under Various Flight Conditions;International Journal of Aeronautical and Space Sciences;2024-07-10

3. Effect of synergistic impact gas injection device on secondary combustion in boron-based ducted rockets;Applied Thermal Engineering;2024-04

4. Study on mixing and combustion characteristics of solid rocket ramjet with a large angle of attack;Aerospace Science and Technology;2023-10

5. Effects of turbulence and flamelet combustion modelling on the CFD simulation of a dual inlet ramjet combustor;International Journal of Turbo & Jet-Engines;2023-09-12

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