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3D CFD Investigation of Low Pressure Turbine Aerodynamics

Sharpe, Jacob Andrew

Abstract Details

2017, Master of Science in Mechanical Engineering (MSME), Wright State University, Mechanical Engineering.
A 3-D Reynolds-Averaged Navier Stokes (RANS) model of a highly-loaded blade profile has been developed using a commercial CFD code with an unstructured/structured grid and several different turbulence models. The ability of each model to predict total pressure loss performance is examined in terms of the spanwise loss distribution and the integrated total pressure loss coefficient. The flowfield predicted by each model is investigated through comparisons of isosurfaces of Q criterion to previous Implicit Large Eddy Simulation (ILES) results. The 3-equation k-kl-¿ model was shown to provide the most accurate performance predictions for a baseline 3-D LPT geometry, and was then used to analyze the effect a new 3D contoured geometry. The model accurately predicted the qualitative improvement made by the contour by weakening the various vortex structures.
Mitch Wolff, Ph.D. (Advisor)
Rolf Sondergaard, Ph.D. (Committee Member)
Rory Roberts, Ph.D. (Committee Member)
81 p.

Recommended Citations

Citations

  • Sharpe, J. A. (2017). 3D CFD Investigation of Low Pressure Turbine Aerodynamics [Master's thesis, Wright State University]. OhioLINK Electronic Theses and Dissertations Center. http://rave.ohiolink.edu/etdc/view?acc_num=wright1495872867696744

    APA Style (7th edition)

  • Sharpe, Jacob. 3D CFD Investigation of Low Pressure Turbine Aerodynamics. 2017. Wright State University, Master's thesis. OhioLINK Electronic Theses and Dissertations Center, http://rave.ohiolink.edu/etdc/view?acc_num=wright1495872867696744.

    MLA Style (8th edition)

  • Sharpe, Jacob. "3D CFD Investigation of Low Pressure Turbine Aerodynamics." Master's thesis, Wright State University, 2017. http://rave.ohiolink.edu/etdc/view?acc_num=wright1495872867696744

    Chicago Manual of Style (17th edition)