Radiative properties of alumina/aluminum particles and influence on radiative heat transfer in solid rocket motor-Reference-Cited by-同舟云学术

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Radiative properties of alumina/aluminum particles and influence on radiative heat transfer in solid rocket motor

Published:2022-02 Issue:2 Volume:35 Page:98-116
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

HAO Xuefan,ZHANG Hu,HOU Xiao,TANG Guihua

Funder

Fundamental Research Funds for the Central Universities

National Natural Science Foundation of China

National Postdoctoral Program for Innovative Talents

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference31 articles.

1. Chemical rocket propulsion: A comprehensive survey of energetic materials;de Luca,2016

2. Geisler R. A global view of the use of aluminum fuel in solid rocket motors. Reston: AIAA; 2002. Report No.: AIAA-2002-3748.

3. Radiative heat feedback in aluminized solid propellant combustion;Brewster;J Thermophys Heat Transf,1988

4. The influence of radiative heat feedback on burning rate in aluminized propellants;Ishihara;Combust Flame,1991

5. Numerical study on similarity of plume infrared radiation between reduced-scale solid rocket motors;Zhang;Chin J Aeronaut,2016

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1. Comprehensive modeling of ignition and combustion of multiscale aluminum particles under various pressure conditions;Chinese Journal of Aeronautics;2024-07

2. Numerical prediction of the two-phase flow and radiation effects on the thermal environment and ablation of solid rocket nozzle;International Journal of Thermal Sciences;2024-03

3. Drag force and heat transfer characteristics of deformable alumina droplets in compressible flows;Physics of Fluids;2024-03-01

4. Elaborative collection of condensed combustion products of solid propellants: Towards a real Solid Rocket Motor (SRM) operational environment;Chinese Journal of Aeronautics;2024-01

5. Atomic insight into the combustion behavior of aluminum nanoparticles under mixed atmosphere of H2O, CO2 and O2;Acta Astronautica;2023-09

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