External Heat Transfer Predictions in a Highly Loaded Transonic Linear Turbine Guide Vane Cascade Using an Upwind Biased Navier–Stokes Solver

Author:

Gehrer A.1,Jericha H.1

Affiliation:

1. Institute of Thermal Turbomachinery and Machine Dynamics, Graz University of Technology, Graz, Austria

Abstract

External heat transfer predictions are performed for two-dimensional turbine blade cascades. The Reynolds-averaged Navier–Stokes equations with algebraic (Arnone and Pacciani, 1998), one-equation (Spalart and Allmaras, 1994), and two-equation (low-Re k–ε, Biswas and Fukuyama, 1994) turbulence closures are solved with a fully implicit time-marching finite volume method. Comparisons with measurements (Arts et al., 1990; Arts, 1994) for a highly loaded transonic turbine nozzle guide vane cascade show good agreement in some cases, but also reveal problems with transition prediction and turbulence modeling. Special attention has been focused on the low-Re k–ε model concerning the influence of the inlet boundary condition for the ε-equation and problems in the stagnation point region.

Publisher

ASME International

Subject

Mechanical Engineering

Reference21 articles.

1. Arnone A. , and PaccianiR., 1998, “IGV–Rotor Interaction Analysis in a Transonic Compressor Using the Navier–Stokes Equations,” ASME JOURNAL OF TURBOMACHINERY, Vol. 120, pp. 147–155.

2. Artner, W., 1997, “Implementierung eines Eingleichungsmodells in einen 2D Navier Stokes Code,” Diploma Thesis, TU-Graz, ITTM.

3. Arts, T., Lambert de Rouvroit, M., and Rutherford, A. W., 1990, “Aero-thermal Investigation of a Highly Loaded Transonic Linear Turbine Guide Vane Cascade,” Technical Note 174, von Karman Institute for Fluid Dynamics, Belgium.

4. Arts, T., 1994, “Highly Loaded Transonic and Film Cooled Linear Turbine Guide Vane Cascade,” in: “Numerical Methods for Flow Calculation in Turbomachines,” VKI Lecture Series, 1994-06.

5. Baldwin, B. S., and Lomax, H., 1978, “Thin layer approximation and algebraic model for separated turbulent flows,” AIAA Paper No. 78-257.

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