Performance Improvement Through Indexing of Turbine Airfoils: Part 2—Numerical Simulation
Author:
Affiliation:
1. Fluid Dynamics Analysis, National Aeronautics and Space Administration, George C. Marshall Space Flight Center, Marshall Space Flight Center, AL 35812
2. Pratt & Whitney, Technical, West Palm Beach, FL 33410; and East Hartford, CT 06108
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/turbomachinery/article-pdf/118/4/636/5593976/636_1.pdf
Reference12 articles.
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3. Griffin, L. W., and Rowey, R. J., 1993, “Analytical Investigation of the Unsteady Aerodynamic Environments in Space Shuttle Main Engine (SSME) Turbines,” ASME Paper No. 93-GT-362.
4. Gundy-Burlet, K. L., Rai, M. M., and Dring, R. P., 1989, “Two-Dimensional Computations of Multi-stage Compressor Flows Using a Zonal Approach,” AIAA Paper No. 89-2452.
5. Gundy-Burlet K. L. , RaiM. M., StauterR. C., and DringR. P., 1991, “Temporally and Spatially Resolved Flow in a Two-Stage Axial Compressor: Part II—Computational Assessment,” ASME JOURNAL OF TURBOMACHINERY, Vol. 113, pp. 227–232.
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