NASA NTRS · 19820018423
Comparison of Experimental and Analytical Performance for Contoured Endwall Stators
Abstract
Comparisons between predicted and experimental stator losses showed that the analysis was able to predict the change in stator loss when contoured endwalls with highly three dimensional passage geometry were used. The level of loss was predicted to within 75 percent of that measured. The predicted loss was due only to profile loss and boundary layer growth on the endwalls. The 25 percent difference was approximately 0.015 at design pressure ratio. The analysis was shown to predict the trend in stator flow angle, even for small stator geometries.
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Boyle, R. J., Haas, J. E.. 1982-01-01. Comparison of Experimental and Analytical Performance for Contoured Endwall Stators. https://ntrs.nasa.gov/citations/19820018423
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