航天器环境工程
航天器環境工程
항천기배경공정
SPACECRAFT ENVIRONMENT ENGINEERING
2014年
5期
483-488
,共6页
推力器%羽流%热效应%Knudsen模型
推力器%羽流%熱效應%Knudsen模型
추력기%우류%열효응%Knudsen모형
thruster%plume%heating effect%Knudsen model
开展羽流热效应计算模型精确评估是合理进行热控设计的前提和条件。文章采用数值求解N-S方程和基于工程经验的点源法相结合的方法得到羽流内外流场;而后采用理论经验公式对羽流热效应计算模型中的关键参数(壁面热适应系数)进行分析,并讨论它们的取值范围;最后利用MBB 10 N推力器的地面试验数据,对羽流热效应关键参数的取值范围进行了精确评估,使得羽流热效应计算误差减小到工程允许的范围内,确认了修正后计算模型的正确性和可信度。
開展羽流熱效應計算模型精確評估是閤理進行熱控設計的前提和條件。文章採用數值求解N-S方程和基于工程經驗的點源法相結閤的方法得到羽流內外流場;而後採用理論經驗公式對羽流熱效應計算模型中的關鍵參數(壁麵熱適應繫數)進行分析,併討論它們的取值範圍;最後利用MBB 10 N推力器的地麵試驗數據,對羽流熱效應關鍵參數的取值範圍進行瞭精確評估,使得羽流熱效應計算誤差減小到工程允許的範圍內,確認瞭脩正後計算模型的正確性和可信度。
개전우류열효응계산모형정학평고시합리진행열공설계적전제화조건。문장채용수치구해N-S방정화기우공정경험적점원법상결합적방법득도우류내외류장;이후채용이론경험공식대우류열효응계산모형중적관건삼수(벽면열괄응계수)진행분석,병토론타문적취치범위;최후이용MBB 10 N추력기적지면시험수거,대우류열효응관건삼수적취치범위진행료정학평고,사득우류열효응계산오차감소도공정윤허적범위내,학인료수정후계산모형적정학성화가신도。
The verification and the evaluation of the plume heating model are important for the reasonable thermal control design. In this paper, the numerical simulations through the N-S equation and the source flow method combined with the engineering empirical results are carried out to calculate the plume flow field. The critical parameter (the wall accommodation ratio) of the plume heating model is analyzed based on the theoretical formula. The experimental heat flux data of the MBB 10 N bipropellant thruster are used to analyze and improve the accuracy of the plume heating model. Based on the ergodic searching of the critical parameter of the plume heating model, the proper range of the wall accommodation ratio is discussed for engineering calculations and applications. By using the modified plume heating model, the accuracy and the reliability of the calculation results are improved and the plume heat evaluation error for engineering designs is in the tolerance range.