推进技术
推進技術
추진기술
JOURNAL OF PROPULSION TECHNOLOGY
2015年
4期
579-586
,共8页
杨金广%刘振德%邵伏永%吴虎
楊金廣%劉振德%邵伏永%吳虎
양금엄%류진덕%소복영%오호
叶轮机械%气动设计%反方法%总切向力%渗透边界条件
葉輪機械%氣動設計%反方法%總切嚮力%滲透邊界條件
협륜궤계%기동설계%반방법%총절향력%삼투변계조건
Turbomachinery%Aerodynamic design%Inverse method%Total tangential force%Transpiration boundary condition
通过集总参数分析,发现确定了反方法的定解条件——总切向力与出口气流角的关系。进而表明在多数情况下,反方法有两个物理解存在,而最终收敛到哪个解由渗透边界条件与定解条件的相容性决定。为了保证基于渗透边界条件的反方法收敛到期望解,文中基于质量流量强加的概念提出了一种处理措施,并通过例子验证了该措施的有效性。最后利用所发展的准三维反方法对跨声速压气机叶栅进行改型设计,效率增加了1.4%,展现了反方法在控制轴向载荷分布方面的优越性。
通過集總參數分析,髮現確定瞭反方法的定解條件——總切嚮力與齣口氣流角的關繫。進而錶明在多數情況下,反方法有兩箇物理解存在,而最終收斂到哪箇解由滲透邊界條件與定解條件的相容性決定。為瞭保證基于滲透邊界條件的反方法收斂到期望解,文中基于質量流量彊加的概唸提齣瞭一種處理措施,併通過例子驗證瞭該措施的有效性。最後利用所髮展的準三維反方法對跨聲速壓氣機葉柵進行改型設計,效率增加瞭1.4%,展現瞭反方法在控製軸嚮載荷分佈方麵的優越性。
통과집총삼수분석,발현학정료반방법적정해조건——총절향력여출구기류각적관계。진이표명재다수정황하,반방법유량개물리해존재,이최종수렴도나개해유삼투변계조건여정해조건적상용성결정。위료보증기우삼투변계조건적반방법수렴도기망해,문중기우질량류량강가적개념제출료일충처리조시,병통과례자험증료해조시적유효성。최후이용소발전적준삼유반방법대과성속압기궤협책진행개형설계,효솔증가료1.4%,전현료반방법재공제축향재하분포방면적우월성。
By a lumped parameters analysis,it is found that the solution determination condition of the in?verse method can be expressed by function between outlet flow angle and total tangential force ,and in most case there are two physical solutions. The converged solution is determined by the consistence of the transpiration boundary condition and the solution determination condition. A technique is developed to force the solution con?verged to a desired solution. The developed Q3D design system is validated by a transonic compressor cascades case,and a 1.4%efficiency gain is obtained,which demonstrate the power of the inverse method to control the axi?al distribution of the pressure loading.