End wall loss reduction of high lift low pressure turbine airfoils using profile contouring—Part II: validation

Authors

• Keith Sangston, University of Arizona
• Jesse Little, University of Arizona
• M. Eric Lyall, Air Force Research Laboratory
• Rolf Sondergaard, Air Force Research Laboratory

Document Type

Article

Publication Date

8-2014

Comments

Note: This article has no AFIT authors, but is included in AFIT Scholar because it is part II of an article sequence in Journal of Turbomachinery, cited elsewhere in the Faculty Publications collection. Click here for the citation record to the earlier article.

Copyright © 2014 by ASME

The full article is available from ASME via subscription or purchase, using the DOI link below.

DOI

10.1115/1.4025952

Source Publication

Journal of Turbomachinery (ISSN 0889-504X | eISSN 1528-8900)

Recommended Citation

Sangston, K., Little, J., Lyall, M. E., and Sondergaard, R. (January 31, 2014). "End Wall Loss Reduction of High Lift Low Pressure Turbine Airfoils Using Profile Contouring—Part II: Validation." ASME. J. Turbomach. August 2014; 136(8): 081006. https://doi.org/10.1115/1.4025952