Sheilla N Torres-Nieves, Ph.D
Associate Professor
Fluid Dynamics and Turbulence
Office: L-217
sheilla.torres@upr.edu
T: 787-832-4040x
Education
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Rensselaer Polytechnic Institute, Troy, New York, USA, 2011 |
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Rensselaer Polytechnic Institute, Troy, New York, USA, 2007 |
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Universidad de Puerto Rico, Mayagüez, Puerto Rico, 2005 |
Background
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Associate Professor, Department of Mechanical Engineering, University of Puerto Rico at Mayagüez |
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Senior Engineer, Compression Systems Aerodynamics, Pratt and Whitney, Connecticut, USA |
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Aerodynamics Discipline Lead for Advanced Commercial Gen2 Fan Rig, Pratt and Whitney Connecticut, USA |
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Visiting Scholar, Department of Mechanical Engineering, The Johns Hopkins University, Baltimore, Maryland |
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Research Assistant, Department of Mechanical Engineering, Rensselaer Polytechnic Institute, Troy, NY |
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Visiting Research Scholar, Department of Mechanical Engineering, The Johns Hopkins University, Baltimore, Maryland |
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Undergraduate Research Program, Department of Mechanical Engineering, University of Puerto Rico at Mayagüez and Boeing Co. |
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Special Undergraduate Project, Department of Mechanical Engineering, University of Puerto Rico at Mayagüez |
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Research and Development Internship, General Motors Corp., Pontiac, Michigan |
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Undergraduate Research Program, Department of Mechanical Engineering, University of Puerto Rico at Mayagüez and Boeing Co. |
Academic and Professional Leadership
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Conference Publications
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Major Peer-Reviewed Journal Publications
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Distinctions & Awards
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Modeling of turbulence realistic atmospheric turbulent boundary layer conditions for a wind turbine in a scaled-down wind tunnel
Design of a fractal and strakes to generate turbulence and simulate the atmospheric boundary layer inside a wind tunnel to understand the effect on wind turbines.
Experimental Study on the Effects of External Conditions on Boundary Layers of Adjacent Blades
Design of experimental setup to study boundary layer development on adjacent blades to simulate compressor airfoils in gas turbines. Design of experimental setup to understand the individual and joint effects of multiple external conditions on endwall boundary layers.
Boundary Layers affected by Pressure Fields of Adjacent Compressor Blades: A Numerical Approach
Computational simulation of a compressor cascade to study boundary layer development on compressors in gas turbines.