化工学报
化工學報
화공학보
CIESC Jorunal
2015年
11期
4312-4319
,共8页
湿蒸汽%跨声速%两相流%凝结%热力学%激波
濕蒸汽%跨聲速%兩相流%凝結%熱力學%激波
습증기%과성속%량상류%응결%열역학%격파
wet steam%transonic%two-phase flow%condensation%thermodynamics%shock wave
水蒸气凝结两相流动呈现高度的非平衡特性。目前,凝结参数都是利用半经验公式得出,很少考虑两相间传热温差以及耦合问题。在湿蒸汽两相流输运方程的基础上,建立了一种准确简单的凝结成核和水滴生长模型,采用具有较好激波捕获效果的高精度二阶 TVD 格式进行离散,计算了湿蒸汽非平衡凝结流动参数及凝结冲波分布。着重研究了湿蒸汽非平衡凝结流动的热力学特性,讨论了进口压力对凝结特性的影响,归纳了进口过冷度对成核率、水滴数、凝结冲波形态的变化规律。研究表明:进口压力增加,凝结位置逐渐向上游移动;进口过冷度降低,凝结位置向下游移动,达到较高的 Mach 数后,才会出现凝结成核;进口过冷度越高,非平衡凝结相变产生的湿度越高。凝结冲波出现后,湿蒸汽沿喷管继续高速流动,其流动规律与等熵流动相似。
水蒸氣凝結兩相流動呈現高度的非平衡特性。目前,凝結參數都是利用半經驗公式得齣,很少攷慮兩相間傳熱溫差以及耦閤問題。在濕蒸汽兩相流輸運方程的基礎上,建立瞭一種準確簡單的凝結成覈和水滴生長模型,採用具有較好激波捕穫效果的高精度二階 TVD 格式進行離散,計算瞭濕蒸汽非平衡凝結流動參數及凝結遲波分佈。著重研究瞭濕蒸汽非平衡凝結流動的熱力學特性,討論瞭進口壓力對凝結特性的影響,歸納瞭進口過冷度對成覈率、水滴數、凝結遲波形態的變化規律。研究錶明:進口壓力增加,凝結位置逐漸嚮上遊移動;進口過冷度降低,凝結位置嚮下遊移動,達到較高的 Mach 數後,纔會齣現凝結成覈;進口過冷度越高,非平衡凝結相變產生的濕度越高。凝結遲波齣現後,濕蒸汽沿噴管繼續高速流動,其流動規律與等熵流動相似。
수증기응결량상류동정현고도적비평형특성。목전,응결삼수도시이용반경험공식득출,흔소고필량상간전열온차이급우합문제。재습증기량상류수운방정적기출상,건립료일충준학간단적응결성핵화수적생장모형,채용구유교호격파포획효과적고정도이계 TVD 격식진행리산,계산료습증기비평형응결류동삼수급응결충파분포。착중연구료습증기비평형응결류동적열역학특성,토론료진구압력대응결특성적영향,귀납료진구과랭도대성핵솔、수적수、응결충파형태적변화규률。연구표명:진구압력증가,응결위치축점향상유이동;진구과랭도강저,응결위치향하유이동,체도교고적 Mach 수후,재회출현응결성핵;진구과랭도월고,비평형응결상변산생적습도월고。응결충파출현후,습증기연분관계속고속류동,기류동규률여등적류동상사。
Wet steam condensation flows presents a high degree of non-equilibrium characteristics. At present, the condensation parameters are obtained by using semi-empirical formula, while heat transfer temperature difference and coupling problems are seldom considered. A simple condensation nucleation model and droplet growth model for non-equilibrium phase change of wet steam is established in this study. In order to calculate the wet steam parameters and condensation shock wave distribution of non-equilibrium condensation flows, the second-order TVD scheme is adopted. The influence of thermodynamic properties of inlet wet steam on the non-equilibrium condensation flow is examined, the influence of inlet pressure on the condensation characteristic is discussed, and various patterns of inlet subcooled temperature on nucleation rate, droplet number, condensation shock are summarized. It is found that as inlet pressure increases, the condensing location moves upstream. At a lower import subcooled temperature, the condensing position moves downstream. At higher Mach number, nucleation occurs. As the import subcooled temperature increase, the wetness of non-equilibrium condensation phase transition will be higher. After the onset of condensation shock, steam expands continuously along the nozzle and the flow pattern is similar to isentropic flow.