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激波对超声速气膜冷却流动换热特性影响研究 推进技术[1001-4055], Published 2023, Volume 44, Issue 2, Pages 122-132
气膜冷却温度场预测的标通量模型评估研究 工程热物理学报[0253-231X], Published 2023, Volume 44, Issue 2, Pages 342-348
Near-wall turbulent transport mechanisms in a micro-ribb e d channel INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER[0017-9310], Published 2022, Volume 188,
气膜冷却圆孔射流输运特性的大涡模拟研究 工程热物理学报[0253-231X], Published 2022, Issue 3, Pages 46-55
Development trends in high-efficiency gas turbine cooling methods 燃气涡轮高效冷却技术及设计方法发展趋势 Qinghua Daxue Xuebao/Journal of Tsinghua University[1000-0054], Published 2022, Volume 62, Issue 4, Pages 794-801
Flow and heat transfer characteristics in a pre-swirl rotor-stator cavity International Journal of Thermal Sciences[1290-0729], Published 2022, Volume 172,
Derivation of a continuous adjoint topology optimization method applied on heat transfer for incompressible flow Numerical Heat Transfer; Part A: Applications[1040-7782], Published 2022, Volume 83, Issue 10, Pages 1067-1079
Flow and heat transfer characteristics of Coriolis-utilization rotating rectangular smooth cooling U-channel APPLIED THERMAL ENGINEERING[1359-4311], Published 2022, Volume 211,
Data-Driven Conjugate Heat Transfer Analysis of a Gas Turbine Vane PROCESSES[2227-9717], Published 2022, Volume 10, Issue 11,
DEVELOPING A SCALAR FLUX MODEL SOLELY BASED ON MEAN FLOW QUANTITIES FOR THE FILM COOLING JET FLOW Proceedings of the ASME Turbo Expo, Published 2022, Volume 6-A,
Numerical study of using dean vortices to enhance the film cooling performance for fan shaped hole INTERNATIONAL JOURNAL OF THERMAL SCIENCES[1290-0729], Published 2021, Volume 165,
Effects of varying non-axisymmetric contours of the turbine endwall on aerodynamics and heat transfer Aspects:A sensitivity analysis study International Journal of Thermal Sciences[1290-0729], Published 2021, Volume 161,
Multi-objective optimization of non-axisymmetric contoured endwall for axial turbines International Journal of Gas Turbine, Propulsion and Power Systems[1882-5079], Published 2021, Volume 12, Issue 1,
Adiabatic effectiveness and heat transfer measurements of simple and trenched cylindrical holes with backward injection INTERNATIONAL JOURNAL OF THERMAL SCIENCES[1290-0729], Published 2021, Volume 170,
Experimental Investigation of Micro Cooling Units on Impingement Jet Array Flow Pressure Loss and Heat Transfer Characteristics ENERGIES, Published 2021, Volume 14, Issue 16,
Effect of leakage flow on the endwall cooling performance in high subsonic turbine cascade International Journal of Thermal Sciences[1290-0729], Published 2021, Volume 170,
The interaction between upstream and downstream film cooling rows in flow field and heat transfer International Journal of Thermal Sciences[1290-0729], Published 2020, Volume 149,
Enhancement of Film Cooling Effectiveness Using Dean Vortices JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME[0889-504X], Published 2020, Volume 142, Issue 1,
基于响应面法的气膜冷却几何参数敏感性分析 工程热物理学报[0253-231X], Published 2020, Volume 41, Issue 05, Pages 1126-1132
Full coverage film cooling on a non-axisymmetric contoured endwall and the baseline endwall International Journal of Thermal Sciences[1290-0729], Published 2020, Volume 158,
静叶端壁耦合传热的分析方法 工程热物理学报[0253-231X], Published 2019, Volume 40, Issue 01, Pages 55-59
Conjugate heat transfer characteristics in a highly thermally loaded film cooling configuration with TBC in syngas Aerospace[2226-4310], Published 2019, Volume 6, Issue 2,
On improving full-coverage effusion cooling efficiency by varying cooling arrangements and wall thickness in double wall cooling application Journal of Heat Transfer[0022-1481], Published 2019, Volume 141, Issue 4,
Split of heat transfer regions and flow characteristics of perforated blockages with inclined holes for trailing edge cooling Numerical Heat Transfer; Part A: Applications[1040-7782], Published 2019, Volume 75, Issue 1, Pages 21-39
Wall thickness and injection direction effects on flat plate full-coverage film cooling arrays: Adiabatic film effectiveness and heat transfer coefficient International Journal of Thermal Sciences[1290-0729], Published 2019, Volume 136, Pages 172-181
Influence of endwall 2D contouring on endwall adiabatic cooling effectiveness and aerodynamic performance INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER[0017-9310], Published 2019, Volume 137, Pages 690-702
Cooling effectiveness and aerodynamic performance in a 2D-Contoured endwall passage with different mass flow ratios INTERNATIONAL JOURNAL OF THERMAL SCIENCES[1290-0729], Published 2019, Volume 142, Pages 233-246
燃气轮机透平叶片国产化需解决的关键技术问题 燃气轮机技术[1009-2889], Published 2019, Issue 02, Pages 1-7
Heat Transfer Characteristics of Inclined Impingement and Pin-Fin Cooling Structure Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics[0253-231X], Published 2019, Volume 40, Issue 2, Pages 389-395
Influence of Combustor Outlet Profile on a Contoured Vane Endwall Cooling Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics[0253-231X], Published 2019, Volume 40, Issue 1, Pages 191-197
Uncertainty quantification of the effects of small manufacturing deviations on film cooling: A fan-shaped hole Aerospace[2226-4310], Published 2019, Volume 6, Issue 4,
Flow and heat transfer characteristics of micro pin-fins under jet impingement arrays International Journal of Heat and Mass Transfer[0017-9310], Published 2019, Volume 143,
Effect of axial turbine non-axisymmetric endwall contouring on film cooling at different locations International Journal of Heat and Mass Transfer[0017-9310], Published 2019, Volume 147,
Enhancement of film cooling effectiveness using Dean vortices Proceedings of the ASME Turbo Expo, Published 2019, Volume 5A-2019,
Superposition characteristics of full coverage film cooling with various blowing ratio and row number Proceedings of the ASME Turbo Expo, Published 2019, Volume 5B-2019,
Influence of simplifications of blade in gas turbine on film cooling performance APPLIED THERMAL ENGINEERING[1359-4311], Published 2018, Volume 128, Pages 877-886
High resolution measurements of film cooling performance of simple and compound angle cylindrical holes with varying hole length-to-diameter ratio-Part I: Adiabatic film effectiveness INTERNATIONAL JOURNAL OF THERMAL SCIENCES[1290-0729], Published 2018, Volume 124, Pages 146-161
Influence of coolant mass flow rate on the endwall conjugate heat transfer International Journal of Thermal Sciences[1290-0729], Published 2018, Volume 129, Pages 416-425
A Novel Method for Designing Fan-Shaped Holes With Short Length-to-Diameter Ratio in Producing High Film Cooling Performance for Thin-Wall Turbine Airfoil JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME[0889-504X], Published 2018, Volume 140, Issue 9,
微小扰流元件对阵列冲击冷却流动换热的影响 工程热物理学报[0253-231X], Published 2018, Volume 39, Issue 07, Pages 1447-1452
Effects of endwall 3d contouring on film cooling effectiveness of cylindrical hole injections at different locations on vane endwall Proceedings of the ASME Turbo Expo, Published 2018, Volume 5C-2018,
Effect of row spacing on the accuracy of film cooling superposition method Proceedings of the ASME Turbo Expo, Published 2018, Volume 5C-2018,
On improving full-coverage effusion cooling efficiency by varying cooling arrangements and wall thickness in double wall cooling application Proceedings of the ASME Turbo Expo, Published 2018, Volume 5A-2018,
Numerical study on local heat transfer in a rotating cooling channel Proceedings of the ASME Turbo Expo, Published 2018, Volume 5A-2018,
Length to diameter ratio effect on heat transfer performance of simple and compound angle holes in thin-wall airfoil cooling International Journal of Heat and Mass Transfer[0017-9310], Published 2018, Volume 127, Pages 867-879
Experimental investigation of wall thickness and hole shape variation effects on full-coverage film cooling performance for a gas turbine vane Applied Thermal Engineering[1359-4311], Published 2018, Volume 144, Pages 349-361
High resolution heat transfer measurements of cylindrical holes embedded in a trench with backward injection Proceedings of the ASME Turbo Expo, Published 2018, Volume 5C-2018,
Influences of micro pin-fin on jet array impingement heat transfer: Effects of jet to target distance, micro pin-fin shapes, height, and reynolds number Proceedings of the ASME Turbo Expo, Published 2018, Volume 5A-2018,
Experimental Investigation of Local and Average Heat Transfer Coefficients Under an Inline Impinging Jet Array, Including Jets With Low Impingement Distance and Inclined Angle JOURNAL OF HEAT TRANSFER-TRANSACTIONS OF THE ASME[0022-1481], Published 2017, Volume 139, Issue 1,
Effect of Reynolds Number, Hole Patterns, and Hole Inclination on Cooling Performance of an Impinging Jet Array-Part I: Convective Heat Transfer Results and Optimization JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME[0889-504X], Published 2017, Volume 139, Issue 4,
Large eddy simulation of compound angle hole film cooling with hole length-to-diameter ratio and internal crossflow orientation effects INTERNATIONAL JOURNAL OF THERMAL SCIENCES[1290-0729], Published 2017, Volume 121, Pages 410-423
综合冷却效率多参数影响分析 工程热物理学报[0253-231X], Published 2017, Volume 38, Issue 12, Pages 2720-2724
On the flow structures and adiabatic film effectiveness for simple and compound angle hole with varied length-to-diameter ratio by Large Eddy simulation and pressure-sensitive paint techniques Journal of Heat Transfer[0022-1481], Published 2017, Volume 139, Issue 12,
Experimental Investigation of Endwall Heat Transfer With Film and Impingement Cooling Journal of Engineering for Gas Turbines and Power[0742-4795], Published 2017, Volume 139, Issue 10,
Effect of Reynolds number, hole patterns, and target plate thickness on the cooling performance of an impinging jet array-part II: Conjugate heat transfer results and optimization Journal of Turbomachinery[0889-504X], Published 2017, Volume 139, Issue 10,
The Flow and Heat Transfer Characteristics of a Impinging Cooling Structure Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics[0253-231X], Published 2017, Volume 38, Issue 7, Pages 1577-1582
Flow Characteristics and Superposition Rule of Two Rows of Round Holes Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics[0253-231X], Published 2017, Volume 38, Issue 5, Pages 1082-1086
Numerical investigation of coolant-to-mainstream scaling parameters with film cooling on pressure and suction side of a gas turbine blade Proceedings of the ASME Turbo Expo, Published 2017, Volume 5A-2017,
Heat transfer coefficients of forward & backward cylindrical hole film cooling using transient ir technique Proceedings of the ASME Turbo Expo, Published 2017, Volume 5C-2017,
Numerical investigation on the effect of slot leakage on a NGV with 2D contoured endwall: Adiabatic effectiveness and aerodynamic loss Proceedings of the ASME Turbo Expo, Published 2017, Volume 5B-2017,
Effect of holes shape on cooling performance of trailing edge of gas turbine blade with perforated blockages with inclined holes Proceedings of the ASME Turbo Expo, Published 2017, Volume 5A-2017,
On the reliability of RANS turbulence models for endwall cooling prediction Proceedings of the ASME Turbo Expo, Published 2017, Volume 5A-2017,
Large eddy simulation of axial and compound angle holes with varying hole length-to-diameter ratio Proceedings of the ASME Turbo Expo, Published 2017, Volume 5A-2017,
Uncertainty quantification of conjugate heat transfer of a cooled turbine vane: Roughness effect Proceedings of the ASME Turbo Expo, Published 2017, Volume 5A-2017,
Multi-row film cooling characteristics on a vane endwall INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER[0017-9310], Published 2016, Volume 92, Pages 23-33
Assessment of six turbulence models for modeling and predicting narrow passage flows, part1: Impingement jets NUMERICAL HEAT TRANSFER PART A-APPLICATIONS[1040-7782], Published 2016, Volume 69, Issue 2, Pages 109-127
Assessment of six turbulence models for modeling and predicting narrow passage flows, part 2: Pin fin arrays NUMERICAL HEAT TRANSFER PART A-APPLICATIONS[1040-7782], Published 2016, Volume 69, Issue 5, Pages 445-463
Effect of thermal boundary conditions and thermal conductivity on conjugate heat transfer performance in pin fin arrays INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER[0017-9310], Published 2016, Volume 95, Pages 579-592
Geometrical Optimization and Experimental Validation of a Tripod Film Cooling Hole With Asymmetric Side Holes JOURNAL OF HEAT TRANSFER-TRANSACTIONS OF THE ASME[0022-1481], Published 2016, Volume 138, Issue 6,
Conjugate Heat Transfer Characteristics of a Highly Thermal-Loaded Film Cooling System in Hot and Multicomposition Gas Condition JOURNAL OF HEAT TRANSFER-TRANSACTIONS OF THE ASME[0022-1481], Published 2016, Volume 138, Issue 2,
Influence of different film cooling arrangements on endwall cooling INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER[0017-9310], Published 2016, Volume 102, Pages 348-359
Effects of wall curvature and streamwise pressure gradient on film cooling effectiveness APPLIED THERMAL ENGINEERING[1359-4311], Published 2016, Volume 107, Pages 776-784
OVERALL COOLING EFFECTIVENESS ON A FLAT PLATE WITH BOTH FILM COOLING AND IMPINGEMENT COOLING IN HOT GAS CONDITION PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2016, VOL 5A, Published 2016,
INFLUENCE OF TOPOLOGY ON HEAT TRANSFER IN A DOUBLE WALL COOLING CHANNEL: POTENTIAL OF SERIES-LINKED JETS PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2016, VOL 5B, Published 2016,
EFFECT OF REYNOLDS NUMBER, HOLE PATTERNS AND HOLE INCLINATION ON COOLING PERFORMANCE OF AN IMPINGING JET ARRAY, PART I: CONVECTIVE HEAT TRANSFER RESULTS AND OPTIMIZATION PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2016, VOL 5B, Published 2016,
EFFECT OF REYNOLDS NUMBER, HOLE PATTERNS, TARGET PLATE THICKNESS ON COOLING PERFORMANCE OF AN IMPINGING JET ARRAY: PART II - CONJUGATE HEAT TRANSFER RESULTS AND OPTIMIZATION PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2016, VOL 5B, Published 2016,
Use of pressure measurements to determine effectiveness of turbine rim seals. Journal of Engineering for Gas Turbines and Power[0742-4795], Published 2015, Volume 137, Issue 3,
整级透平中转静轮缘封严问题研究partⅱ:不同封严结构的特性 工程热物理学报[0253-232X], Published 2015, Volume 36, Issue 3, Pages 496-500
Optimal Arrangement of Combined-Hole for Improving Film Cooling Effectiveness JOURNAL OF THERMAL SCIENCE AND ENGINEERING APPLICATIONS[1948-5085], Published 2015, Volume 7, Issue 1,
Unsteady Structure and Development of a Row of Impingement Jets, Including Kelvin-Helmholtz Vortex Development JOURNAL OF FLUIDS ENGINEERING-TRANSACTIONS OF THE ASME[0098-2202], Published 2015, Volume 137, Issue 5,
Effects of compound angle on film cooling effectiveness with different streamwise pressure gradient and convex curvature INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER[0017-9310], Published 2015, Volume 86, Pages 482-491
Film cooling effectiveness distribution of cylindrical hole injections at different locations on a vane endwall INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER[0017-9310], Published 2015, Volume 90, Pages 1-14
Application of algebraic anisotropic turbulence models to film cooling flows INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER[0017-9310], Published 2015, Volume 91, Pages 7-17
Algebraic anisotropic turbulence modeling of compound angled film cooling validated by particle image velocimetry and pressure sensitive paint measurements JOURNAL OF HEAT TRANSFER-TRANSACTIONS OF THE ASME[0022-1481], Published 2014, Volume 136, Issue 3, Pages -
Analysis and optimization of interaction between endwall flank flow and turbine rotor-stator rim seal Tuijin Jishu/Journal of Propulsion Technology[1001-4055], Published 2014, Volume 35, Issue 6, Pages 758-765
Assesment of six turbulence models for pin fin arrays of blade trailing edge Proceedings of 5th ISJPPE, Published 2014,
Combined effects of perforated blockages and pin fins in a trailing edge internal cooling duct Proceedings of the ASME Turbo Expo[978-0-791-84571-4], Published 2014, Volume 5A,
Coupled aerothermodynamics optimization for the cooling system of a turbine vane Journal of Turbomachinery[0889-504X], Published 2014, Volume 136, Issue 5,
Effect of Corrugated Orifice and Pin-Fin on Multiple Array Impingement Cooling with Low Nozzle to Target Distance Proceedings of the ASME Turbo Expo[978-0-791-84571-4], Published 2014, Volume 5A,
Effect of Radiative Heat Transfer Factors on Temperature Distribution of a First Stage Vane Proceedings of the ASME Turbo Expo[978-0-791-84572-1], Published 2014, Volume 5B,
Experimental and numerical investigation of unsteady impingement cooling within a blade leading edge passage International Journal of Heat and Mass Transfer[0017-9310], Published 2014, Volume 71, Pages 57-68
Experimental investigations of sycee film coolng performance on a plate and a tested vane of an F-Class gas turbine Proceedings of the ASME Turbo Expo[978-0-791-84572-1], Published 2014, Volume 5B,
Film cooling modeling of turbine blades using algebraic anisotropic turbulence models Journal Of Turbomachinery-Transactions Of The Asme[0889-504X], Published 2014, Volume 136, Issue 11,
Geometrical optimization and experimental validation of a tripod film cooling hole with asymmetric side holes Proceedings of the ASME Turbo Expo[978-0-791-84572-1], Published 2014, Volume 5B,
Heat transferring of channels with repeated ribs in turbine blades Part II: Conjugate heat transfer characteristics Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics[0253-231X], Published 2014, Volume 35, Issue 1, Pages 42-45
Optimization of the hole exit shaping of film holes without and with compound angles for maximal film cooling effectiveness Proceedings of the ASME Turbo Expo[978-0-791-84572-1], Published 2014, Volume 5B,
Phantom cooling of nozzle trailing edge discharge on blade surface and platform Proceedings of the ASME Turbo Expo[978-0-791-84572-1], Published 2014, Volume 5B,
Prediction of 3D Unsteady Flow and Heat Transfer in Rotating Cavity by Discontinuous Galerkin Method and Transition Model ASME Turbo Expo 2014[978-0-791-84572-2], Published 2014,
Rotor-stator rim seal analysis in one stage gas turbine Part I: Ingestion and seal Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics[0253-231X], Published 2014, Volume 35, Issue 5, Pages 873-877
Status and development trend of the heavy duty gas turbine Zhongguo Dianji Gongcheng Xuebao/Proceedings of the Chinese Society of Electrical Engineering[0258-8013], Published 2014, Volume 34, Issue 29, Pages 5096-5102
Total hemispherical radiation properties of oxidized nickel at high temperatures Corrosion Science[0010-938X], Published 2014,
Turbulence modeling of film cooling with algebraic anisotropic turbulent scalar-flux correction Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics[0253-231X], Published 2014, Volume 35, Issue 2, Pages 247-251
主流流向压力梯度对气膜冷却效率的影响 工程热物理学报[0253-233X], Published 2014, Volume 35, Issue 3, Pages 461-464
低ma数预处理间断有限元方法研究 清华大学学报[1000-0054], Published 2014,
冲击冷却对燃气轮机尾缘双流程内冷通道传热和压损的影响 工程热物理学报[0253-231X], Published 2014, Volume 35, Issue 7, Pages 1295-1299
叶片双层冷却单元的修正一维模型 工程热物理学报[0253-231X], Published 2014, Volume 35, Issue 10, Pages 1943-1946
各向异性涡黏模型在通道分离流动中的应用 工程热物理学报[0253-231X], Published 2014, Volume 35, Issue 9, Pages 1727-1732
多场耦合下透平冷却高温影响特性 工程热物理学报[0253-231X], Published 2014, Volume 35, Issue 8, Pages 1513-1516
带标量修正的气膜冷却各向异性湍流模型 工程热物理学报[0253-231X], Published 2014, Issue 2,
气膜冷却布置对前缘流动传热的影响 工程热物理学报[0253-231X], Published 2014, Volume 35, Issue 12, Pages 2372-2375
燃机叶片平行肋扰流内冷通道传热特性研究part2:耦合传热特性 工程热物理学报[0253-231X], Published 2014, Issue 1,
端壁侧向出流对透平轮缘密封的影响及优化 推进技术[1001-4055], Published 2014, Issue 6,
透平静叶前缘和压力面气膜冷却实验研究 清华大学学报(自然科学版)[1000-0054], Published 2014, Volume 54, Issue 6, Pages 769-774
间断galerkin方法在气冷透平流热耦合计算中的应用 广东电力[1007-290X], Published 2014, Volume 27, Issue 11, Pages 1-5
Algebraic anisotropic turbulence modeling of compound angled film cooling validated by PIV and PSP measurements Proceedings of the ASME Turbo Expo[978-0-791-85515-7], Published 2013, Volume 3, Issue 3,
Cooling structure optimization for a rib-roughed channel in a turbine rotor blade Proceedings of the ASME Turbo Expo, Published 2013, Volume 3,
Coupled aero-thermodynamics optimization for the cooling system of a turbine vane Proceedings of the ASME Turbo Expo, Published 2013, Volume 3,
Effect of film cooling arrangement on impingement heat transfer on turbine blade leading edge Proceedings of the ASME Turbo Expo, Published 2013, Volume 3,
Effect of inlet swirl on the model leading edge of turbine vane Proceedings of the ASME Turbo Expo[978-0-7918-5523-2], Published 2013, Volume 6,
Effect of RIB configuration and lateral ejection on a high aspect ratio trailing edge channel Proceedings of the ASME Turbo Expo[978-0-791-85514-0], Published 2013, Volume 3,
Effects of swirlers arrangement on gas turbine combustion chamber flow field International Conference on Power Engineering 2013, ICOPE 2013, Published 2013,
Experimental and numerical study of the anti-crossflows impingement cooling structure INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER[0017-9310], Published 2013, Volume 64, Pages 567-580
Heat transfer character of film cooling combined with TBCs in hot and multi-composition gas condition Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics[0253-231X], Published 2013, Volume 34, Issue 7, Pages 1251-1255
Heat transfer characteristics of film cooling in the non-transparent gas environment Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics[0253-231X], Published 2013, Volume 34, Issue 2, Pages 249-252
Heat transferring of channels with repeated ribs in turbine blades part1: Mechanism of flow and convective heat transfer Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics[0253-231X], Published 2013, Volume 34, Issue 4, Pages 624-627
Influence of different turbulence models in predicting convective heat transfer in a cascade Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics[0253-231X], Published 2013, Volume 34, Issue 6, Pages 1042-1046
Optimal arrangement of combined-hole for improving film cooling effectiveness Proceedings of the ASME Turbo Expo, Published 2013, Volume 3,
Unsteady characteristic of film cooling and phantom cooling on the first stage of a gas turbine: Part 1 - Vane cascade Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics[0253-231X], Published 2013, Volume 34, Issue 5, Pages 845-848
Unsteady characteristic of film cooling and phantom cooling on the first stage of a gas turbine: Part 2 - Blade cascade Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics[0253-231X], Published 2013, Volume 34, Issue 12, Pages 2258-2261
不同湍流模型对叶栅对流传热预测的影响 工程热物理学报[0253-231X], Published 2013, Issue 6,
全矩阵无积分间断有限元实现 中国科技论文[2095-2783], Published 2013, Volume 8, Issue 8, Pages 776-779
扇形孔气膜冷却应用的综合特性 工程热物理学报[0253-231X], Published 2013, Volume 34, Issue 1, Pages 55-58
扇形孔气膜冷却应用的综合特性 - characteristics of fan shaped hole film cooling 工程热物理学报[0253-231X], Published 2013, Volume 34, Issue 1,
燃机叶片平行肋扰流内冷通道传热特性研究Part Ⅰ:流动传热机理 工程热物理学报[0253-231X], Published 2013, Issue 4,
燃气轮机一级透平动静叶交互作用的气膜非定常特性及泛冷却效应:Part 1-静叶栅 工程热物理学报[0253-231X], Published 2013, Issue 5,
燃气轮机内部冷却瞬态液晶技术的误差分析 工程热物理学报[0253-231X], Published 2013, Volume 34, Issue 8, Pages 1444-1448
燃气轮机内部冷却瞬态液晶技术的误差分析 - uncertainties of the transient thermochromic liquid crystal method in gas turbine internal cooling measurements 工程热物理学报[0253-231X], Published 2013, Volume 34, Issue 8,
非透明气体环境中气膜冷却的流热特性 工程热物理学报[0253-231X], Published 2013, Issue 2,
高温多组分工况下气膜冷却及tbcs传热特性 工程热物理学报[0253-231X], Published 2013, Issue 7,
Application of the anisotropic eddy-viscosity model to film cooling flows with different geometries Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics[0253-231X], Published 2012, Volume 33, Issue 4, Pages 578-582
Application of transient liquid crystal on internal cooling research of gas turbine airfoil Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics[0253-231X], Published 2012, Volume 33, Issue 4, Pages 665-669
Effect of the hot gas composition on a highly thermally loaded film cooling system PROCEEDINGS OF THE ASME TURBO EXPO 2011, VOL 5, PTS A AND B, Published 2012, Pages 335-344
Effects of inlet swirl condition on the flow and heat transfer performance of gas turbine vane Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics[0253-231X], Published 2012, Volume 33, Issue 11, Pages 1868-1871
Full field algebraic anisotropic eddy viscosity model for the film cooling flows Proceedings of the ASME Turbo Expo, Published 2012, Volume 4, Issue PARTS A AND B, Pages 1421-1430
Heat transfer characteristic of rotor-stator system with small radial outflow Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics[0253-231X], Published 2012, Volume 33, Issue 7, Pages 1122-1126
Multi-dimensional platform for cooling design of air-cooled turbine blades Proceedings of the ASME Turbo Expo, Published 2012, Volume 4, Issue PARTS A AND B, Pages 207-218
Multi-parameter influence on combined-hole film cooling system INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER[0017-9310], Published 2012, Volume 55, Issue 15-16, Pages 4232-4240
Multi-parameter influence on film cooling of blade tip Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics[0253-231X], Published 2012, Volume 33, Issue 9, Pages 1501-1504
Radiation effectiveness on the AERO- and thermodynamics in a highly thermally loaded film cooling system PROCEEDINGS OF THE ASME TURBO EXPO 2011, VOL 5, PTS A AND B, Published 2012, Pages 325-334
Radiative models for hot gas with various H2O-CO2 ratios Proceedings of the ASME Turbo Expo, Published 2012, Volume 4, Issue PARTS A AND B, Pages 1041-1049
Research on the effect of combustor outlet radiation on the film cooling heat transfer Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics[0253-231X], Published 2012, Volume 33, Issue 2, Pages 214-217
多参数对叶顶气膜冷却的影响 工程热物理学报[0253-231X], Published 2012, Issue 9,
多参数影响下的气膜冷却特性及预测方法 - prediction methods and performance of film cooling influenced by Multi-Parameters 热力透平[1672-5549], Published 2012, Volume 41, Issue 1,
小流量下的转静系盘腔传热特征分析 - heat transfer characteristic of Rotor-Stator system with small radial outflow 工程热物理学报[0253-231X], Published 2012, Volume 33, Issue 7,
旋流条件对燃气轮机叶片流动传热特性的影响 工程热物理学报[0253-231X], Published 2012, Issue 11,
湍流黏性修正在不同孔型气膜计算中的应用 - application of the anisotropic Eddy-Viscosity model to film cooling flows with different geometries 工程热物理学报[0253-231X], Published 2012, Volume 33, Issue 4,
燃气轮机二次空气系统一维传热特性预测 - prediction of the secondary air system＇ s 1d heat transfer characteristics in the gas turbine 热力透平[1672-5549], Published 2012, Volume 41, Issue 2,
燃烧室出口辐射对气膜冷却传热影响研究 - research on the effect of combustor outlet radiation on the film cooling heat transfer 工程热物理学报[0253-231X], Published 2012, Volume 33, Issue 2,
瞬态液晶技术在涡轮叶片内部冷却研究中的应用 - application of transient liquid crystal on internal cooling research of gas turbine airfoil 工程热物理学报[0253-231X], Published 2012, Volume 33, Issue 4,
Aero-and thermodaynamic features of the flow fields in the internal cooling channels with film cooling holes Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics[0253-231X], Published 2011, Volume 32, Issue 8, Pages 1385-1388
Algebraic anisotropic eddy-viscosity modeling for application to turbulent film cooling flows Proceedings of the ASME Turbo Expo[978-0-791-85465-5], Published 2011, Volume 5, Issue PTS A AND B, Pages 379-388
Effect of Turning Vane Configurations on Heat Transfer and Pressure Drop in a Ribbed Internal Cooling System JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME[0889-504X], Published 2011, Volume 133, Issue 4, Pages -
Effects of density ratio and blowing ratio on the film cooling effectiveness on a turbine vane Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics[0253-231X], Published 2011, Volume 32, Issue 8, Pages 1295-1298
Improved eddy-viscosity modelling of film cooling flows Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics[0253-231X], Published 2011, Volume 32, Issue 4, Pages 573-576
Prediction of the adiabatic film cooling effectiveness influenced by multi parameters based on BP neural network Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics[0253-231X], Published 2011, Volume 32, Issue 7, Pages 1127-1130
Sequential algorithm based flexible-fuel gas turbine thermodynamic analysis Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics[0253-231X], Published 2011, Volume 32, Issue 1, Pages 29-32
先进燃气轮机的特征及发展趋势 Published 2011,
基于bp神经网络的多参数气膜冷却效率研究 - prediction of the adiabatic film cooling effectiveness influnenced by multi parameters based on bp neural network 工程热物理学报[0253-231X], Published 2011, Volume 32, Issue 7,
基于顺序算法的灵活燃料燃气轮机气动热力性能分析 - sequential algorithm based FLEXIBLE-FUEL gas turbine thermodynamic analysis 工程热物理学报[0253-231X], Published 2011, Volume 32, Issue 1,
密度比和吹风比对透平静叶气膜冷却的影响 - effects of density ratio and blowing ratio on the film cooling effectiveness on a turbine vane 工程热物理学报[0253-231X], Published 2011, Volume 32, Issue 8,
带气膜孔内部冷却通道的流动传热特性 - Aero-and thermodaynamic features of the flow fields in the internal cooling channels with film cooling holes 工程热物理学报[0253-231X], Published 2011, Volume 32, Issue 8,
气膜冷却计算中湍流黏性系数的修正 - improved Eddy-Viscosity modelling of film cooling flows 工程热物理学报[0253-231X], Published 2011, Volume 32, Issue 4,
Aero-thermo dynamical characteristics in a ribbed trapezoidal internal cooling system Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics[0253-231X], Published 2010, Volume 31, Issue 5, Pages 753-756
Characteristic of double-jet film cooling tested by pressure sensitive paint Hangkong Dongli Xuebao/Journal of Aerospace Power[1000-8055], Published 2010, Volume 25, Issue 12, Pages 2770-2778
Effects of radiative heat transfer on a highly thermal loaded film cooled plate Proceedings of 3rd ISJPPE, Published 2010,
Experimental and numerical investigation of conjugate heat transfer to a high temperature flat plate with film cooling Qinghua Daxue Xuebao/Journal of Tsinghua University[1000-0054], Published 2010, Volume 50, Issue 12, Pages 1988-1993
Experimental investigation of heat transfer and pressure drop in a two-pass internal coolant passages of gas turbine airfoil Hangkong Dongli Xuebao/Journal of Aerospace Power[1000-8055], Published 2010, Volume 25, Issue 12, Pages 2779-2786
Film cooling performance of the embedded holes in trenches with compound angles PROCEEDINGS OF THE ASME TURBO EXPO 2010, VOL 4, PTS A AND B, Published 2010, Pages 1415-1424
Optimization of gas turbine performance based on low-Btu fuels Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics[0253-231X], Published 2010, Volume 31, Issue 8, Pages 1303-1306
基于psp实验技术的双射流气膜冷却特性研究 - characteristic of double-jet film cooling tested by pressure sensitive paint 航空动力学报[1000-8055], Published 2010, Issue 12,
基于压敏漆的带横槽气膜冷却实验与数值研究 - film cooling performance of the embedded holes in trenches with compound angles 工程热物理学报[0253-231X], Published 2010, Issue 2,
梯形带肋内部冷却通道的流动及传热特性 - AERO-THERMO dynamical characteristics in a ribbed trapezoidal internal cooling system 工程热物理学报[0253-231X], Published 2010, Issue 5,
涡轮叶片内部冷却通道传热和压力分布特性的实验 - experimental investigation of heat transfer and pressure drop in a two-pass internal coolant passages of gas turbine airfoil 航空动力学报[1000-8055], Published 2010, Issue 12,
燃气轮机燃用中低热值燃料性能优化方案研究 - optimization of gas turbine performance based on LOW-BTU fuels 工程热物理学报[0253-231X], Published 2010, Issue 8,
燃气轮机高温叶片气膜冷却系统的研究进展 - recent progress on gas turbine film cooling research 热力透平[1672-5549], Published 2010, Volume 39, Issue 1,
高温平板气膜冷却耦合换热实验与计算 - experimental and numerical investigation of conjugate heat transfer to a high temperature flat plate with film cooling 清华大学学报：自然科学版[1000-0054], Published 2010, Issue 12,
Application of γ-Reθ transition model for internal cooling simulation Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics[0253-231X], Published 2009, Volume 30, Issue 11, Pages 1849-1852
How far have we been? – summary of the investigation on rotating cavity at idg, rwth aachen uni. - Frontiers of Energy and Power Engineering in China.[1673-7393], Published 2009, Volume 3, Issue 4, Pages 489-497
Numerical investigation of flow and heat transfer in a rotating cavity with axial throughflow Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics[0253-231X], Published 2009, Volume 30, Issue 7, Pages 1129-1131
Prediction of flow features in rotating cavities with axial throughflow by rans and les PROCEEDINGS OF THE ASME TURBO EXPO 2009, VOL 3, PTS A AND B, Published 2009, Pages 1173-1181
Verification of rans for analyzing convective cooling system with and without ribs PROCEEDINGS OF THE ASME TURBO EXPO 2009, VOL 3, PTS A AND B, Published 2009, Pages 409-420
γ-Re_θ转捩模型在内部冷却叶片中的应用 工程热物理学报[0253-231X], Published 2009, Issue 11,
γ-Reθ转捩模型在内部冷却叶片中的应用 - application of γ-Reθ transition model for internal cooling simulation 工程热物理学报[0253-231X], Published 2009, Issue 11,
超超临界汽轮机高温部件材料和冷却技术之探讨 - advanced materials and cooling technologies for high thermal load components in ultra supercritical steam turbine 热力透平[1672-5549], Published 2009, Volume 38, Issue 1,
轴向通流旋转盘腔中流动与传热数值研究 - numerical investigation of flow and heat transfer in a rotating cavity with axial throughflow 工程热物理学报[0253-231X], Published 2009, Issue 7,
How far have we been? --Summary of investigations on rotating cavity at IDG, RWTH Aachen University.(Report) 2nd International Symposium on Jet Propulsion and Power Engineering (ISJPPE), Published 2007,
Investigation of the steam-cooled blade in a steam turbine cascade Hangkong Dongli Xuebao/Journal of Aerospace Power[1000-8055], Published 2007, Volume 22, Issue 5, Pages 673-682
Parameter survey of thermally highly loaded, porous and cooled multi-layer systems for turbine blades JOURNAL OF THERMAL SCIENCE[1003-2169], Published 2007, Volume 16, Issue 2, Pages 181-185
Investigation of the unstable flow structure in a rotating cavity Proceedings of the ASME Turbo Expo 2006, Vol 3, Pts A and B: HEAT TRANSFER: GENERAL INTEREST, Published 2006, Pages 1433-1442
Cooling performance of the steam-cooled vane in a steam turbine cascade Proceedings of the ASME Turbo Expo 2005, Vol 3 Pts A and B, Published 2005, Pages 217-226
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