哈尔滨工程大学学报
哈爾濱工程大學學報
합이빈공정대학학보
JOURNAL OF HARBIN ENGINEERING UNIVERSITY
2014年
8期
948-953
,共6页
付丽荣%张文平%明平剑%罗跃生
付麗榮%張文平%明平劍%囉躍生
부려영%장문평%명평검%라약생
柴油机%辐射%三维数值模拟%有限体积法%缸内%热流量%燃烧室%换热
柴油機%輻射%三維數值模擬%有限體積法%缸內%熱流量%燃燒室%換熱
시유궤%복사%삼유수치모의%유한체적법%항내%열류량%연소실%환열
diesel engines%radiation%three dimensional numerical simulation%finite volume method%in-cylinder%heat flux%combustor%heat transfer
为了在自主开发的通用流体力学数值模拟软件GTEA上进行柴油机缸内辐射换热三维数值模拟,假设柴油机缸内气体为漫灰介质,基于非结构有限体积法( UFVM),研究了空间的非散射性辐射问题以及辐射换热三维数值计算方法。对六面体、圆柱体进行辐射换热数值方法验证,分析了不同的网格离散和立体角离散对计算结果的影响,并用此方法研究了TBD620型柴油机ω型燃烧室的辐射换热。结果表明:数值结果与精确解和文献中方法的结果吻合较好;当网格离散和立体角离散满足一定的对应关系时,才能得到更精确的计算结果;燃烧室中工质的吸收系数和温度对缸壁的热流量有一定的影响。
為瞭在自主開髮的通用流體力學數值模擬軟件GTEA上進行柴油機缸內輻射換熱三維數值模擬,假設柴油機缸內氣體為漫灰介質,基于非結構有限體積法( UFVM),研究瞭空間的非散射性輻射問題以及輻射換熱三維數值計算方法。對六麵體、圓柱體進行輻射換熱數值方法驗證,分析瞭不同的網格離散和立體角離散對計算結果的影響,併用此方法研究瞭TBD620型柴油機ω型燃燒室的輻射換熱。結果錶明:數值結果與精確解和文獻中方法的結果吻閤較好;噹網格離散和立體角離散滿足一定的對應關繫時,纔能得到更精確的計算結果;燃燒室中工質的吸收繫數和溫度對缸壁的熱流量有一定的影響。
위료재자주개발적통용류체역학수치모의연건GTEA상진행시유궤항내복사환열삼유수치모의,가설시유궤항내기체위만회개질,기우비결구유한체적법( UFVM),연구료공간적비산사성복사문제이급복사환열삼유수치계산방법。대륙면체、원주체진행복사환열수치방법험증,분석료불동적망격리산화입체각리산대계산결과적영향,병용차방법연구료TBD620형시유궤ω형연소실적복사환열。결과표명:수치결과여정학해화문헌중방법적결과문합교호;당망격리산화입체각리산만족일정적대응관계시,재능득도경정학적계산결과;연소실중공질적흡수계수화온도대항벽적열류량유일정적영향。
The three-dimensional numerical simulation of the radiation heat transfer of the diesel engine in-cylinder was performed with the general fluid flow numerical simulation solver-GTEA, which was developed independently by us. The gas used in the diesel engine cylinder was assumed to be grey medium. In this study, a three-dimension-al numerical method is proposed for the spatial non-scattering radiation problem, which is based on the unstructured finite volume method ( UFVM) . For its validation, a hexahedral enclosure and a cylinder enclosure were presented. The influence of different discrete meshes and solid angles on the computational results was investigated. Then, the radiation heat transfer in the combustor of the TBD620 diesel engines was studied with the present numerical meth-od. It was found that all the results obtained by the presented FVM approach match exactly with the solutions and results of the literature. For getting more accurate results, discrete meshes and solid angles should satisfy certain re-lationships. The absorption coefficient and temperatures of the medium have certain effects on the radiation heat flux of the wall of the combustion chamber.