火箭推进
火箭推進
화전추진
JOURNAL OF ROCKET PROPULSION
2011年
6期
52-60,66
,共10页
朱子勇%孙万民%王占林
硃子勇%孫萬民%王佔林
주자용%손만민%왕점림
LH2贮箱%置换%数值模拟
LH2貯箱%置換%數值模擬
LH2저상%치환%수치모의
LH2 tank%replacement%numerical calculation
首先应用C#软件编制贮箱气体置换计算程序,用该程序对不同N2、H2充气压力和放气终压对贮箱置换的影响进行分析,通过对比分析得出最优置换方案;其次利用FLU—ENT软件对某运载火箭发动机动力系统试验LH2贮箱气体置换过程进行数值计算,包括N2充气置换、H2充气置换和LH2贮箱缩比尺寸和全尺寸数值计算。对H2置换过程中不同的放气终压也进行了数值计算,并将缩比尺寸数值计算结果同现有试验台LH2贮箱置换进行比较;最后数值计算了LH2贮箱H2充气完成后混合均匀需要的时间。
首先應用C#軟件編製貯箱氣體置換計算程序,用該程序對不同N2、H2充氣壓力和放氣終壓對貯箱置換的影響進行分析,通過對比分析得齣最優置換方案;其次利用FLU—ENT軟件對某運載火箭髮動機動力繫統試驗LH2貯箱氣體置換過程進行數值計算,包括N2充氣置換、H2充氣置換和LH2貯箱縮比呎吋和全呎吋數值計算。對H2置換過程中不同的放氣終壓也進行瞭數值計算,併將縮比呎吋數值計算結果同現有試驗檯LH2貯箱置換進行比較;最後數值計算瞭LH2貯箱H2充氣完成後混閤均勻需要的時間。
수선응용C#연건편제저상기체치환계산정서,용해정서대불동N2、H2충기압력화방기종압대저상치환적영향진행분석,통과대비분석득출최우치환방안;기차이용FLU—ENT연건대모운재화전발동궤동력계통시험LH2저상기체치환과정진행수치계산,포괄N2충기치환、H2충기치환화LH2저상축비척촌화전척촌수치계산。대H2치환과정중불동적방기종압야진행료수치계산,병장축비척촌수치계산결과동현유시험태LH2저상치환진행비교;최후수치계산료LH2저상H2충기완성후혼합균균수요적시간。
The program of gas replacement in the tank is drawn up with C# NET software. The influence of different filling pressure and final pressure after deflation of nitrogen and hydrogen on gas replacement in the tank is analyzed with the program. An optimum scheme of gas replacement is determined by comprehensive comparison. The numerical calculation of gas replacement process in the liquid hydrogen testing tank of a rocket engine power system is carried out with FLUENT software. The numerical calculation includes the nitrogen filling replacement, hydrogen filling replacement, downsizing scaling and full-size liquid hydrogen tank. The results of numerical calculation are compared with the replacement of existing liquid hydrogen tank on the test-bed. The duration time of the gas mixing uniformity after completion of the hydrogen filling is calculated.