Improving the completeness of combustion of boron particles in a solid-fuel ducted rocket owing to distributed air supply to the secondary combustor

Rashkovskii S. A.; Milekhin Yu. M.; Fedorychev A. V.

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Improving the completeness of combustion of boron particles in a solid-fuel ducted rocket owing to distributed air supply to the secondary combustor

机译：由于向二次燃烧器分配了空气，提高了固体燃料管道火箭中硼颗粒燃烧的完整性。

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A model of combustion of boron particles in ducted rocket using distributed air supply to the secondary combustor was developed for the first time. The completeness of boron combustion in ducted rocket using air supply to the secondary combustor through one outlet or two outlets (distributed air supply) was calculated. It was shown that, in some cases, distributed air supply significantly (by a factor of 1.5-3) decreases the time of complete combustion of boron particles and thereby increases the completeness of fuel combustion in ducted rocket. The modeling results agree with the known experimental data.

机译：首次建立了利用向次级燃烧器分配空气的管道火箭中硼颗粒燃烧的模型。计算了通过使用一个或两个出口向次级燃烧室供气（分布式供气）的管道火箭中硼燃烧的完整性。结果表明，在某些情况下，分布式空气供应（以1.5-3的倍数）显着减少了硼颗粒完全燃烧的时间，从而增加了管式火箭燃料燃烧的完整性。建模结果与已知实验数据吻合。

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《Doklady Physical Chemistry》 |2016年第2期|共5页
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Rashkovskii S. A.; Milekhin Yu. M.; Fedorychev A. V.;
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正文语种 eng
中图分类物理化学（理论化学）、化学物理学;
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1. Improving the completeness of combustion of boron particles in a solid-fuel ducted rocket owing to distributed air supply to the secondary combustor [J] . Rashkovskii S. A., Milekhin Yu. M., Fedorychev A. V. Doklady Physical Chemistry . 2016,第Pta2期

机译：由于向二次燃烧器分配了空气，提高了固体燃料管道火箭中硼颗粒燃烧的完整性。
2. Improved combustion model of boron particles for ducted rocket combustion chambers [J] . Kalpakli Bora, Acar Emir Bedig, Ulas Abdullah Combustion and Flame . 2017,第maya期

机译：管式火箭燃烧室硼粒子燃烧模型的改进
3. Effect of distributed injection of air into the afterburning chamber of a ram-rocket engine on the efficiency of combustion of boron particles [J] . Rashkovskii S. A., Milekhin Yu M., Fedorychev A. V. Combustion, Explosion, and Shock Waves . 2017,第6期

机译：分布式注入空气进入拉力火箭发动机燃烧型硼粒颗粒效率的效果
4. Improving Combustion of Boron Particles in Secondary Combustor of Ducted Rockets [C] . T. Miyayama, H. Oshima, S. Toshiyuki, AIAA/ASME/SAE/ASEE Joint Propulsion Conference Exhibit . 2006

机译：改进管式火箭二次燃烧器中硼粒子的燃烧
5. Performance prediction of a ducted rocket combustor. [D] . Stowe, Robert. 2001

机译：管式火箭燃烧器的性能预测。
6. Research Opportunities for Cancer Associated with Indoor Air Pollution from Solid-Fuel Combustion [O] . Britt C. Reid, Armen A. Ghazarian, David M. DeMarini, 2012

机译：固体燃料燃烧与室内空气污染相关的癌症研究机会
7. Experimental Investigation and Numerical Simulation of Secondary Combustor Flow in Boron-Based Propellant Ducted Rocket [O] . Jianxin HU, Zhixun XIA, Dequan WANG, 2013

机译：硼基推进剂管火箭中二次燃烧器流动的实验研究与数值模拟
8. Combustion of Boron in Airbreathing Rockets: Effects of the Secondary Combustion Chamber [R] . Boussios, A. 1979

机译：空气呼吸火箭中硼的燃烧：二次燃烧室的影响

Improving the completeness of combustion of boron particles in a solid-fuel ducted rocket owing to distributed air supply to the secondary combustor

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