|***** Foxridge Ln, Apt I |Song Xue, Ph.D. |01-540-***-**** |

|Blacksburg, VA 24060 | |abgnxw@r.postjobfree.com |

|Objective |An engineering/research position in Aerodynamics/ Heat |

| |Transfer/ CFD/ Mechanical Design/ Thermal System |

|Summary |

|More than 4 years of experience in heat transfer and aerodynamic experiment in|

|the transonic cascade wind tunnel. More than 3 years of experience in |

|numerical simulation on the flow in turbomachines with commercial codes. |

|Proficient on thermodynamic and aerodynamic experimental equipment and |

|instrumentation. Experienced in CFD analysis of the internal flow. Experienced|

|in mechanical design with CAD tools. Self-motivated researcher with excellent |

|analytical and communication skills. Can work independently as well as a team |

|player. |

| |

|Software skills: |

|CFD software (ANSYS-Fluent, ANSYS-CFX, Numeca); mechanical design code |

|(SolidWorks); data acquisition code (Labview); data processing codes (MATLAB, |

|Mathematics, C |

| |

|Experiment instrumentation skills: |

|Infrared camera on the surface heat transfer measurement; thin film platinum |

|gages on the surface heat transfer measurement; hot-wire probe on turbulence |

|intensity measurement; five hole pressure probe on cascade secondary flow |

|determination. |

|Research Experience |

|Graduate Research Assistant: Transonic Wind Tunnel Lab at Virginia Tech |

|(Blacksburg, VA) |

|May 2008 - Aug 2012 |

|Advisor: Dr. Wing Ng & Dr. Srinath Ekkad |

|Experimental and numerical research on heat transfer in the tip gap region of |

|a gas turbine blade, Jan 2011 - present. (sponsored by Solar Turbines |

|Incorporated) |

|Actions |

| |

|Mentor undergraduate student using SolidWorks (CAD software) to fabricate |

|squealer tip blade with a 3D printing technology, and to conduct the |

|mechanical safety inspection; |

|Guide Master degree candidate using infrared (IR) camera to record blade tip |

|heat transfer data, and to analysis the test results; |

|Instrument Thin Film Platinum gages to measure near tip region heat transfer |

|data. |

|Perform conjugate heat transfer simulation with CFD codes to analysis a |

|thermal protection scheme in the turbine blade tip gap region. (ANSYS-Fluent |

|was employed) |

| |

|Outputs |

|The heat transfer characteristics on the turbine blade tip and the near tip |

|region were mapped with the IR measurement data. The physics of the tip gap |

|flow, and its effect on heat transfer were explored. Different tip gap |

|dimensions were compared at multiple main flow Mach numbers, and suggestions |

|were proposed to protect the turbine blade tip from thermal damage. |

|The sponsor (Solar Turbine Inc.) was satisfied with the progress reports, and |

|decided to continuously support further research on tip gap flow with our lab.|

| |

|The results were summarized in the form of a conference paper, and were |

|submitted to the international conference of TURBOEXPO2013. |

| |

|Experimental and CFD investigation on film-cooling performance on gas turbine |

|blade and nozzle guide vane, Jan 2009 - Dec 2010. (sponsored by Solar Turbines|

|Incorporated) |

|Actions |

| |

|Design and set up film cooling test system in turbine cascade wind tunnel; |

|conduct the heat transfer measurement; Processed the data reduction. (Labview |

|codes were written for the DAQ process; Matlab codes were written for data |

|reduction) |

|Performed CFD study to investigate the detail physics on the shock/film |

|cooling interaction. (ANSYS-CFX was employed) |

|Performed Hot-wire probe measurement to determine the freestream turbulence |

|intensity in the linear cascade test section. |

| |

|Outputs |

|The heat transfer coefficient and film cooling effectiveness of a fan-shaped |

|hole injected gas turbine blade was recorded for the first time under a unique|

|flow condition. A novel phenomenon of shock/film cooling interaction was |

|observed in the experiment, and the physics were explored in the numerical |

|study. The suggestions were proposed to optimize the film cooling performance |

|on a gas turbine blade. |

|The sponsor (Solar Turbine Inc.) was satisfied with the final report, and |

|assigned new research projects to our lab. |

|A part of the research was summarized as a journal paper, which was accepted |

|by the ASME Journal of Turbomachinery. Two other journal papers were submitted|

|to the AIAA Journal of Propulsion. The experimental results were presented at |

|the conference of TURBOEXPO in Jun 2011, and AIAA conference in Jan 2012. |

| |

|Determination of the pressure loss caused by the secondary flow in the linear |

|cascade model of a high turning blade with divergent endwall, Sep 2008 - May |

|2009. (sponsored by Siemens) |

|Actions |

| |

|Designed a five-hole pressure probe for supersonic measurement. (Flow strength|

|estimation/safety check was done both manually and using SolidWorks for |

|special test conditions) |

|Conducted the five-hole pressure probe measurement and data reduction for the |

|total pressure loss determination. (3D interpolation method was coded in |

|Matlab to reduce the pressure data) |

|Designed step motor driving traverse mechanism for the probe moving in the |

|test section to perform multiple location measurement. |

| |

|Outputs |

|The pressure loss caused by the secondary flow at the exit of a gas turbine |

|blade cascade was determined into a 2-D contour map. The result was used to |

|optimize the geometry of the endwall contour in a gas turbine blade cascade. |

|The sponsor (Siemens) was satisfied with the progress report, and decided to |

|continuously support further research. |

|The results were presented at the conference of ASME 2010 3rd Joint |

|US-European Fluids Engineering Summer Meeting. |

| |

| |

|Graduate Research Assistant: Solar Energy Lab in Chinese Academy of Science |

|(Beijing, China) |

|Apr 2006 - Apr 2007 |

|Advisor: Dr. Zhifeng |

|Wang |

|Experimental and numerical investigations of wind effect in the heliostats |

|field of a solar tower plant (supported by Natural Science Foundation of |

|China) |

|Actions |

| |

|Performed CFD investigation on the wind flow in a heliostats field. (Phoenix |

|codes was employed in CFD study) |

|Assist the wind tunnel experiment to measure the pressure distribution on the |

|heliostat surface. |

| |

|Outputs |

|Literature research of the wind effect on the heliostats was complete. The |

|preliminary CFD result was reported. |

|The pressure distribution on the heliostats front and back surface was |

|recorded at different attacking angles and different wind speeds. |

|The principal advisor/manager was convinced to cancel the further research |

|project of the wind effect on heliostats. |

| |

| |

|Graduate Research Assistant: School of Jet Propulsion in Beijing University of|

|Aeronautics and Astronautics (Beijing, China) |

| |

|Jun 2003 - Apr 2006 |

|Advisor: Dr. Xingmin |

|Gui |

|Designed and conducted CFD simulation of mini size rotary pump for artificial |

|heart or left ventricular assist device, Aug 2003 - Apr 2006. (collaborated |

|with Fuwai Hospital) |

|Actions |

| |

|Performed CFD investigation on the mini size rotary pump for artificial heart |

|or left ventricular assist device; designed and improved the rotor blade and |

|the stator vane profiles; developed a 2-D through flow code as a tool for the |

|blade profile design. (Numeca codes was employed) |

|Invented the outer bearing rotary pump for low hemolysis artificial heart. |

|(The bearing was designed outside of the rotor for better powering, improved |

|cooling and lubricating conditions, and eliminating tip gap flow) |

| |

|Outputs |

|The original design of a blood pump for the artificial heart was improved |

|based on the result of the numerical simulation. |

|A patent was awarded for the novel design of the outer bearing blood pump. |

|The progress report in the form of a proposal convinced the National Natural |

|Science Foundation of China to support further research. |

|The research was published as a technical paper in the journal of Artificial |

|Organs in 2007. |

| |

|Teaching Experience |

|Instructor: Course of Engineering Design and Economics, at Virginia Tech |

|(Blacksburg, VA) |

|Aug 2011 - Dec 2011 |

|Lecture a class of 30 students (sophomore level) |

|Topics include product design & engineering economics |

|Education |

|Virginia Polytechnic Institute and State University | Jun 2012 |

|(Blacksburg, Virginia) | |

|Ph.D. in Mechanical Engineering | |

|Total GPA: 3.81/4.0 | |

|Dissertation: Fan-Shaped Hole Film Cooling on Turbine| |

|Blade and Vane in a Transonic Cascade with High | |

|Freestream Turbulence | |

|Beijing University of Aeronautics and Astronautics |Apr 2006 |

|(Beijing, China) | |

|M.S. in Aerospace Propulsion Theory and Engineering | |

|Thesis: Study and design on a low hemolysis axial blood | |

|pump | |

| | |

|Beijing University of Aeronautics and Astronautics |Jun 2003 |

|(Beijing, China) | |

|B.S. in Thermal Energy and Power Engineering | |

|Publications |

|S. Xue, W. Ng, H.K. Moon and L. Zhang. "Fan-Shaped Hole Film Cooling on |

|Turbine Blade in a Transonic Cascade with High Freestream Turbulence," 50th |

|AIAA Aerospace Sciences Meeting, Nashville Tennessee, Jan 2012, |

|AIAA-2012-0368. |

| |

|S. Xue, A. Newman, W. Ng, H.K. Moon and L. Zhang. "Heat Transfer Performance |

|of a Showerhead and Shaped Hole Film Cooled Vane at Transonic Conditions," |

|accepted by ASME Journal of Turbomachinery. (Presented as GT2011-45142 at the |

|Turbo Expo 2011: Power for Land, Sea, and Ai) |

| |

|S. Abraham, K. Panchal, S. Xue, S. V. Ekkad, W. Ng, B. J. Brown, A. Malandra. |

|"Experimental And Numerical Investigations of A Transonic, High Turning |

|Turbine Cascade with A Divergent Endwall," Proceedings of ASME 2010 3rd Joint |

|US-European Fluids Engineering Summer Meeting and 8th International Conference|

|on Nanochannels, Microchannels and Minichannels, FEDSM2010-ICNMM2010. |

| |

|Y. Zhang, S. Xue, X. Gui, H. Sun, H. Zhang, X. Zhu, and S. Hu. "A Novel |

|Integrated Rotor of Axial Blood Flow Pump Designed With Computational Fluid |

|Dynamics," Artificial Organs, 2007, Vol. 31, pp. 580-585. |

| |

|S. Xue, W. Ng, S. V. Ekkad, "Shock effect on fan-shaped film cooled gas |

|turbine blade suction side: CFD and comparison with experiment". (in |

|preparation for a journal submission) |

| |

|K. Anto, S. Xue, W.F. Ng, L.J. Zhang, H.K. Moon, "Effects of Tip Clearance Gap|

|and Exit Mach Number on Turbine Blade Tip and Near-Tip Heat Transfer". |

|(submitted to the ASME Turbo Expo 2013) |

| |

|Chinese Patent: CN1958085 2007-05-09 |

|Title: Outer bearing type artificial heart blood pump |

|Inventor: Song Xue, Yan Zhang, Xingmin Gui et al. |

|Appl. No.: 200610002894.3 |

|Filed: Feb 10, 2006 |

|Field of Search: A61M1/10(2006.01)I |

|Major Courses | |

|Fluid Dynamics |Advanced Instrumentation |

|Turbomachinery |Modeling MEMS & NEMS |

|Computational Fluid Dynamics |Math of Mechanic Engineering Analysis |

|Convective Heat& Mass Transfer |Heat Conduction |

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