[1] Louis J F.Axial Flow Counter-Rotating Turbines[R].ASME 85-GT-218.
[2] Huber F W.Design and Test of a Small Two Stage Counter-Rotating Turbine for Rocket Engine Application[R].AIAA 93-2136.
[3] 季路成,钟文涛,徐建中.关于1+1/2对转涡轮的基本分析和初步设计[J].工程热物理学报,2001,2(02):167-170.
[4] 乔加飞,赵庆军,徐建中.某1+1/2对转涡轮的气动设计及分析[J].工程热物理学报,2011,2(09):1469-1472.
[5] 赵庆军,王会社,赵晓路,等.无导叶对转涡轮三维流场数值分析[J].推进技术,2006,7(02):114-118.(ZHAO Qing-jun, WANG Hui-she, ZHAO Xiao-lu, et al.Three-Dimensional Numerical Investigation of Vaneless Counter-Rotating Turbine[J].Journal of Propulsion Technology, 2006,7(02):114-118.)
[6] 张惠,王会社,徐建中,等.1+1/2对转涡轮高压动叶气膜冷却数值研究[J].工程热物理学报,2008(03):571-573.
[7] 王会社,张惠,赵庆军,等.1+1/2对转涡轮高压动叶顶部间隙流场数值研究[J].工程热物理学报,2007,8(05):751-754.
[8] 雒伟伟,张磊,王会社,等.可调高压导叶对1+1/2对转涡轮性能影响的数值研究[J].航空动力学报,2011,6(12):2741-2748.
[9] 季路成.对转涡轮研究的回顾与展望[J].航空发动机.2006,2(4):49-53.
[10] JI Lu-cheng.Analysis of Technical Challenges in Vaneless Counter-Rotating Turbomachinery [R].ASME 2007-GT-27617.
[11] 刘思永,王屏,方祥军,等.无导叶对转涡轮新技术气动设计探讨[J].燃气涡轮试验与研究.2002,5(1):20-24.
[12] Kurzke J.How to Get Component Maps for Aircraft Gas Turbine Performance Calculation[R].ASME 96-GT-164.
[13] McKinney J S.Simulation of Turbofan Engine, Part I-Description of Method and Balancing Technique[R].AD-825197,7.
[14] Koenig R W,Fishbach L H.GENENG—A Program for Calculating Design and Off-Design Performance for Turbojet and Turbofan Engines[R].NASA TND-6552,2.
[15] Fishbach L H,Koenig R W.GENENG II—A Program for Calculating Design and Off-Design Performance of Two and Three-Spool Turbofans with as Many as Three Nozzle[R].NASA TND-6553,2.
[16] Sellers J F,Daniel C J.DYNGEN—A Program for Calculating Steady-State and Transient Performance of Turbojet and TurboFan Engines[R].NASA TND-7901,5.
[17] 陈玉春,徐思远,杨云铠,等.改善航空发动机特性计算收敛性的方法[J].航空动力学报,2008,3(12):2242-2248.
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