Experimentally Verified Numerical Optimization of a Three-Dimensional Parametrized Turbine Vane With Nonaxisymmetric End Walls
Author:
Affiliation:
1. MTU Aero Engines Aerodynamics Turbine/Compressor (TEAD), Dachauer Str. 665, 80995 München, Germany
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
https://asmedigitalcollection.asme.org/turbomachinery/article-pdf/127/2/380/6837517/380_1.pdf
Reference16 articles.
1. Rechenberg, 1973.
2. LaFleur, R. S., and Langston, L. S., 1993, “Drag Reduction of a Cylinder/Endwall Junction Using the Ice Formation Method,” ASME J. Fluids Eng., 115.
3. Bischoff, H., 1983, Patentschrift DE 3202855 C1, MTU Motoren- und Turbinen Union, Munich.
4. Rose, M. G., 1994, “Non-Axisymmetric Endwall Profiling in the HP NGV’s of an Axial Flow Gas Turbine,” ASME Paper 94-GT-249.
5. Hartland, J. C., Gregory-Smith, D. G., Harvey, N. W., and Rose, M. G., 1999, “Non-Axisymmetric Turbine End Wall Design: Part II Experimental Validation,” ASME Paper 99-GT338.
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