Grid Orthogonality Effects on Predicted Turbine Midspan Heat Transfer and Performance
Author:
Affiliation:
1. NASA Lewis Research Center, Cleveland, OH 44135
2. University of Kansas, Center for Research, Inc., Lawrence, KS 66045
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/turbomachinery/article-pdf/119/1/31/5840312/31_1.pdf
Reference18 articles.
1. Ameri, A. A., and Arnone, A., 1992, “Navier–Stokes Heat Transfer Predictions Using Two-Equation Turbulence Closures,” Paper No. AIAA-92-3067.
2. Arnone A. , LiouM.-S., and PovinelliL. A., 1992, “Navier–Stokes Solution of Transonic Cascade Flows Using Non-Periodic C-Type Grids,” AIAA Journal of Propulsion and Power, Vol. 8, No. 2, pp. 410–417.
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,” von Karman Institute for Fluid Dynamics, Belgium, Technical Note 174.
4. Baldwin, B. S., and Lomax, H., 1978, “Thin-Layer Approximation and Algebraic Model for Separated Turbulent Flows,” Paper No. AIAA-78-257.
5. Boyle, R. J., and Giel, P. W., 1992, “Three-Dimensional Navier–Stokes Heat Transfer Predictions for Turbine Blade Rows,” Paper No. AIAA-92-3068.
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