Performance Improvement Through Indexing of Turbine Airfoils: Part 1—Experimental Investigation
Author:
Affiliation:
1. Pratt & Whitney, Technical, West Palm Beach, FL 33410
2. Pratt & Whitney, Technical, East Hartford, CT 06108
3. National Aeronautics & Space Administration, Marshall Space Flight Center, Huntsville, AL 35812
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/turbomachinery/article-pdf/118/4/630/5593677/630_1.pdf
Reference7 articles.
1. Carter, J. A., 1991, “Blowdown Turbine Test Equipment Design Characteristics,” NASA memo ED35–45–91.
2. Gaddis, S. W., Hudson, S. T., and Johnson, P. D., 1992, “Cold Flow Testing of the Space Shuttle Main Engine Alternate Turbopump Development High Pressure Fuel Turbine Model,” ASME Paper No. 92-GT-280.
3. Kauffman, W. J., Carter, J. A., Heaman, J. P., and Bordelon, W. J., 1992, “The Design and Performance of the Marshall Space Flight Center Turbine Test Equipment,” ASME Paper No. 93-GT-380.
4. Ni, R. H., 1981, “A Multiple-Grid Scheme for Solving the Euler Equations,” AIAA Paper No. 81-1025; AIAA Journal, Vol. 20, No. 11.
5. Ni, R. H., and Bogoian, J. C., 1989, “Prediction of 3D Multistage Turbine Flow Field Using a Multiple-Grid Euler Solver,” AIAA Paper No. 89-0203.
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