固体火箭技术
固體火箭技術
고체화전기술
JOURNAL OF SOLID ROCKET TECHNOLOGY
2014年
6期
797-803
,共7页
李中华%李志辉%吴俊林%彭傲平
李中華%李誌輝%吳俊林%彭傲平
리중화%리지휘%오준림%팽오평
稀薄气体%DSMC方法%两相流%双向耦合%TPMC方法%高空羽流
稀薄氣體%DSMC方法%兩相流%雙嚮耦閤%TPMC方法%高空羽流
희박기체%DSMC방법%량상류%쌍향우합%TPMC방법%고공우류
rarefied gas%DSMC method%two-phase flow%two-way coupled method%TPMC method%plume flow
通过对气?固两相间动量和能量相互作用解耦处理,建立了一种适于模拟真空环境气固两相混合物羽流的DSMC双向耦合算法与固体颗粒空间输运变化特性的TPMC计算技术。仿真了固体火箭发动机两相羽流流场和固体颗粒在远离发动机喷口数十公里空间扩散运动分布特性,通过将计算结果与典型文献结果及理论分析比较确认,证实本文方法的准确可靠性。结果表明,固体颗粒对气相的扩散有一定的阻滞作用;仅在离发动机喷口一定距离,气相对固体颗粒有较大影响,致颗粒温度下降、速度增加;颗粒温度随发动机喷口距离增大而减小,一直要在远离喷口上百公里颗粒温度才随轴向位置趋于平衡,且不同尺寸的颗粒温度差别较大,对指导外层空间高真空环境气固两相羽流传输影响工程研制具有重要意义。
通過對氣?固兩相間動量和能量相互作用解耦處理,建立瞭一種適于模擬真空環境氣固兩相混閤物羽流的DSMC雙嚮耦閤算法與固體顆粒空間輸運變化特性的TPMC計算技術。倣真瞭固體火箭髮動機兩相羽流流場和固體顆粒在遠離髮動機噴口數十公裏空間擴散運動分佈特性,通過將計算結果與典型文獻結果及理論分析比較確認,證實本文方法的準確可靠性。結果錶明,固體顆粒對氣相的擴散有一定的阻滯作用;僅在離髮動機噴口一定距離,氣相對固體顆粒有較大影響,緻顆粒溫度下降、速度增加;顆粒溫度隨髮動機噴口距離增大而減小,一直要在遠離噴口上百公裏顆粒溫度纔隨軸嚮位置趨于平衡,且不同呎吋的顆粒溫度差彆較大,對指導外層空間高真空環境氣固兩相羽流傳輸影響工程研製具有重要意義。
통과대기?고량상간동량화능량상호작용해우처리,건립료일충괄우모의진공배경기고량상혼합물우류적DSMC쌍향우합산법여고체과립공간수운변화특성적TPMC계산기술。방진료고체화전발동궤량상우류류장화고체과립재원리발동궤분구수십공리공간확산운동분포특성,통과장계산결과여전형문헌결과급이론분석비교학인,증실본문방법적준학가고성。결과표명,고체과립대기상적확산유일정적조체작용;부재리발동궤분구일정거리,기상대고체과립유교대영향,치과립온도하강、속도증가;과립온도수발동궤분구거리증대이감소,일직요재원리분구상백공리과립온도재수축향위치추우평형,차불동척촌적과립온도차별교대,대지도외층공간고진공배경기고량상우류전수영향공정연제구유중요의의。
A numerical simulation approach was presented to simulate rarefied two?phase mixture plume flow by applying two?way coupling technique of DSMC method. The interaction between rarefied gas and solid particles was dealt with decoupling compu?tation of momentum and energy exchange between phases. The TPMC computing technology was also developed to solve the space transport characteristics of solid particles in distant field space. The two?phase plume flow field and particle distribution characteris?tics far away from the engine nozzle were simulated by the DSMC and TPMC method. It is indicated that the present methods and models are correct by the comparison of the computed results with the typical confirmed results from the reference and theoretical a?nalysis. There exists some retarded elasticity in gas phase diffusion of solid particles to some extent. From the engine nozzle dis?tance, gas and solid particles have a greater impact caused with temperature drop and increases of the speed of particles. The granu?lar temperature away from the nozzle exit tends to balance, and the particle temperature is very different with different size of parti?cles. It is shown that there are more intensely interaction between phases in case of higher number density, and particle size affects diffusing range and temperature distribution. The results are of great significance to guide the vacuum gas?solid two?phase plume transmission.