Computing Method Investigation and Verification of Gas-Solid Combustion in Magnesium-Aluminum Based Propellant Ducted Rocket
2012 ◽
Vol 503-504
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pp. 490-493
Keyword(s):
The combustion mechanism, which consisting of 22 species and 23 reaction equations, and three discrete models such as inertia, combusting, modification droplet, are employed for the investigation of gas-solid combustion in magnesium-aluminum based propellant ducted rocket based on thermal performance calculation. And path lines, temperature distribution, sediments are discussed after the computing method is validated by direct-connect experimentation and the flow field information, which obtained by numerical method and coincided with currently conclusions. The results indicated that the proposed method is reliable and practicable.
2014 ◽
Vol 8
(1)
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pp. 636-642
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Keyword(s):
2013 ◽
Vol 483
◽
pp. 587-593
2011 ◽
Vol 38
(3)
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pp. 1668-1674
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2009 ◽
Vol 64
(5-6)
◽
pp. 602-614
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Keyword(s):
2017 ◽
Vol 115
◽
pp. 756-773
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Keyword(s):