火箭推进
火箭推進
화전추진
JOURNAL OF ROCKET PROPULSION
2012年
5期
30-36
,共7页
第三流体循环%传热%流阻%仿真
第三流體循環%傳熱%流阻%倣真
제삼류체순배%전열%류조%방진
third fluid circle%heat transfer%flow resistance%simulation
为了提高发动机循环性能,以某发动机设计参数为基础,以R22、乙烷及乙醇3种介质为对象,进行了第三流体循环发动机性能分析。在性能分析过程中,耦合了系统参数平衡计算与身部传热流阻仿真计算结果,力求使分析结果更接近实际情况。分析结果表明,第三流体循环与传统方式相比,可以提供更高的燃烧室压力,其中采用乙烷为循环介质的第三流体循环发动机性能最高。
為瞭提高髮動機循環性能,以某髮動機設計參數為基礎,以R22、乙烷及乙醇3種介質為對象,進行瞭第三流體循環髮動機性能分析。在性能分析過程中,耦閤瞭繫統參數平衡計算與身部傳熱流阻倣真計算結果,力求使分析結果更接近實際情況。分析結果錶明,第三流體循環與傳統方式相比,可以提供更高的燃燒室壓力,其中採用乙烷為循環介質的第三流體循環髮動機性能最高。
위료제고발동궤순배성능,이모발동궤설계삼수위기출,이R22、을완급을순3충개질위대상,진행료제삼류체순배발동궤성능분석。재성능분석과정중,우합료계통삼수평형계산여신부전열류조방진계산결과,력구사분석결과경접근실제정황。분석결과표명,제삼류체순배여전통방식상비,가이제공경고적연소실압력,기중채용을완위순배개질적제삼류체순배발동궤성능최고。
In order to improve the circle performance of engines, according to the design parame- ters of some engines, the performance of third fluid circle engine is analyzed, for which R22, ethane, ethanol, helium are chosen as the mediums. During the analysis, the balance calculation result of sys- tem parameters and simulation result of flow resistance were coupled to make the analysis result clos- er to the fact. The result shows that in comparison with conventional modes, the third fluid circle can offer higher chamber pressure, and the third fluid circle engine which chooses ethane as its circle medium has the best performance.