The mathematical treatments of ignition and combustion of aluminium powder and the heat feedback to burning surface of nitramine propellant are described. The combustion model established thereof can explain the effects of content,particle size and granular distribution of aluminium powder on combustion bhavior of the propellant,and the precision of modeling calculation is increased as well.
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刘德辉.含铝硝胺推进剂燃速计算研究[J].含能材料, 1997, 5(3):109-113. Liu De-hui. A CALCULATION RESEARCH ON BURNING RATE OF ALUMINIZED NITRAMINE PROPELLANT[J]. Chinese Journal of Energetic Materials, 1997, 5(3):109-113.