Numerical investigation of a high-subsonic axial-flow compressor rotor with non-axisymmetric hub endwall
Author:
Publisher
Springer Science and Business Media LLC
Subject
Condensed Matter Physics
Link
http://link.springer.com/content/pdf/10.1007/s11630-010-0014-8.pdf
Reference11 articles.
1. Hartland, J., Gregory-Smith, D. G., Harvey, N. W. and Rose, M. G., “Non-Axisymmetric End Wall Design: Three-Dimensional Linear Design System,” ASME Journal of Turbomachinery, 2000, 122, 278–285.
2. Hartland, J., Gregory-Smith, D. G., Harvey, N. W. and Rose, M. G., “Non-Axisymmetric End Wall Design: Part II. Experimental Validation,” ASME Journal of Turbomachinery, 2000, 122, pp. 286–293.
3. T. J. Praisner, E. Allen-Bradlelly, E. A. Grover, D. C. Knezevici and S. A. Sjolander, “Application of Non-Axisymmetric Endwall Contouring to Conventional and High-lift Turbine Airfoils,” ASME Paper, GT2007-27579.
4. D. C. Knezevici and S. A. Sjolander, “Measurements of Secondary Losses in a Turbine Cascade with the Implementation of Non-axisymmetric End-wall Contouring” ASME Paper, GT2008-51311.
5. Dorfner, C., Nicke, E., and Voss, C., “Axial-Asymmestric Profiled End-wall Design Using Multiobjective Optimization Linked With 3D Rans-Flow-Simulations,” ASME Paper, GT2007-27268.
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