Laser Ignition of Aluminum and Boron Based Powder Systems; Combustion, Explosion, and Shock Waves; Vol. 58, iss. 4

Detaylı Bibliyografya
Parent link:Combustion, Explosion, and Shock Waves
Vol. 58, iss. 4.— 2022.— [P. 422-429]
Yazar: Korotkikh A. G. Aleksandr Gennadievich
Müşterek Yazar: Национальный исследовательский Томский политехнический университет Инженерная школа энергетики Научно-образовательный центр И. Н. Бутакова (НОЦ И. Н. Бутакова)
Diğer Yazarlar: Sorokin I. V. Ivan Viktorovich, Arkhipov V. A. Vladimir Afanasjevich
Özet:Title screen
Powders of various metals and boron are widely used in composite solid propellants to increase the combustion temperature and specific impulse of rocket engines. This paper presents the results of an experimental study of oxidation and ignition of ultrafine Alex aluminum powder, amorphous boron, microsized μμAl aluminum powder, and AlB2 and AlB12 aluminum borides in air. Metal and boron powders are heated and ignited by a CO2 laser in a heat flux density range of 65-190 W/cm2. It is revealed on the basis of thermal analysis data that the powder reactivity parameters are arranged in the following sequence (in descending order of activity): Alex →→ B →→ AlB12 →→ AlB2 →→ μμAl. The total specific heat release and the mass variation rate reach maximum values during the oxidation of amorphous boron and AlB12 aluminum dodecaboride. The Alex, boron, and AlB12 powders are easier to ignite in air under the action of an external radiant source. The power exponent nn in a dependence between the ignition delay time tigntign and the heat flux density tign(q)tign(q) = Aq−nAq−n for the μμAl, AlB2, and AlB12 powders are approximately the same and equal to ≈≈2.0, and it is lower and reaches nn = 1.5 and 1.0 for ultrafine Alex and boron powders, respectively.
Режим доступа: по договору с организацией-держателем ресурса
Dil:İngilizce
Baskı/Yayın Bilgisi: 2022
Konular:
Online Erişim:https://doi.org/10.1134/S0010508222040049
Materyal Türü: MixedMaterials Elektronik Kitap Bölümü
KOHA link:https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=668464

MARC

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200 1 |a Laser Ignition of Aluminum and Boron Based Powder Systems  |d Лазерное зажигание порошковых систем на основе алюминия и бора  |f A. G. Korotkikh, I. V. Sorokin, V. A. Arkhipov 
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300 |a Title screen 
320 |a [References: 21 tit.] 
330 |a Powders of various metals and boron are widely used in composite solid propellants to increase the combustion temperature and specific impulse of rocket engines. This paper presents the results of an experimental study of oxidation and ignition of ultrafine Alex aluminum powder, amorphous boron, microsized μμAl aluminum powder, and AlB2 and AlB12 aluminum borides in air. Metal and boron powders are heated and ignited by a CO2 laser in a heat flux density range of 65-190 W/cm2. It is revealed on the basis of thermal analysis data that the powder reactivity parameters are arranged in the following sequence (in descending order of activity): Alex →→ B →→ AlB12 →→ AlB2 →→ μμAl. The total specific heat release and the mass variation rate reach maximum values during the oxidation of amorphous boron and AlB12 aluminum dodecaboride. The Alex, boron, and AlB12 powders are easier to ignite in air under the action of an external radiant source. The power exponent nn in a dependence between the ignition delay time tigntign and the heat flux density tign(q)tign(q) = Aq−nAq−n for the μμAl, AlB2, and AlB12 powders are approximately the same and equal to ≈≈2.0, and it is lower and reaches nn = 1.5 and 1.0 for ultrafine Alex and boron powders, respectively. 
333 |a Режим доступа: по договору с организацией-держателем ресурса 
461 |t Combustion, Explosion, and Shock Waves 
463 |t Vol. 58, iss. 4  |v [P. 422-429]  |d 2022 
510 1 |a Лазерное зажигание порошковых систем на основе алюминия и бора  |z rus 
610 1 |a электронный ресурс 
610 1 |a труды учёных ТПУ 
610 1 |a powder 
610 1 |a aluminum 
610 1 |a amorphous boron 
610 1 |a aluminum diboride 
610 1 |a aluminum dodecaboride 
610 1 |a oxidation 
610 1 |a ignition delay time 
610 1 |a ignition temperature 
700 1 |a Korotkikh  |b A. G.  |c specialist in the field of power engineering  |c Professor of Tomsk Polytechnic University, Doctor of Physical and Mathematical Sciences  |f 1976-  |g Aleksandr Gennadievich  |3 (RuTPU)RU\TPU\pers\34763  |9 18113 
701 1 |a Sorokin  |b I. V.  |c Specialist in the field of heat and power engineering  |c Engineer of Tomsk Polytechnic University  |f 1992-  |g Ivan Viktorovich  |3 (RuTPU)RU\TPU\pers\45838 
701 1 |a Arkhipov  |b V. A.  |g Vladimir Afanasjevich 
712 0 2 |a Национальный исследовательский Томский политехнический университет  |b Инженерная школа энергетики  |b Научно-образовательный центр И. Н. Бутакова (НОЦ И. Н. Бутакова)  |3 (RuTPU)RU\TPU\col\23504 
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