Heat balance evaluation of double-base solid propellant combustion using thermography and laser heating on a burning surface
Heat balance evaluation of double-base solid propellant combustion using thermography and laser heating on a burning surface
复制标题
使用热成像和激光加热在燃烧表面上评估双基固体推进剂燃烧的热平衡
DOI:
10.1016/j.ast.2015.09.013
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发表时间:
2015
影响因子:
5.6
通讯作者:
Akira Kakami and Takeshi Tachibana
中科院分区:
文献类型:
--
作者:
鈴木宏二郎;難波和也;Akira Kakami and Takeshi Tachibana
A new method is proposed using laser heating and thermography for estimating the heat transfer balance for burning solid propellant: heat production rate on burning surface Q˙ s, heat flux from burning surface to solid phase Λ p, and heat flux rate from flame to burning surface H f. H f is determined from the correlation between burning rate and power density of laser heating on burning surface; Λ p is evaluated using the burning surface temperature measured with thermography. Double-base propellant is tested in a combustion chamber having a laser-introducing window, and is irradiated with an 808-nm laser at laser power densities ranging from 0.3 to 0.8 W/mm 2 with a back-pressure range from 0.02 to 0.60 MPa. The proposed method shows heat flux from burning surface to burning surface H f of 1.7 W/mm 2, heat production rate on burning surface Q˙ s of 4.9 W/mm 2, and heat flux from burning surface to solid phase Λ p of 6.6 W/mm 2 at a back pressure of 0.60 MPa. Laser power attenuation due to the flame is determined to evaluate the influence of laser power attenuation on the estimation of heat flux rate from flame to burning surface. The experiment shows that errors originating from laser power attenuation due to the flame are below 18%.