Heat Release in Turbine Cooling II: Numerical Details of Secondary Combustion Surrounding Shaped Holes

Authors

• Cheng-Xian Lin, University of Tennessee, Knoxville
• Richard J. Holder, University of Tennessee, Knoxville
• Balu Sekar, Air Force Research Laboratory
• Joseph Zelina, Air Force Research Laboratory
• Marc D. Polanka, Air Force Institute of TechnologyFollow
• Hugh J. Thornburg, Mississippi State University
• Alejandro M. Briones, University of Dayton Research Institute

Document Type

Article

Publication Date

3-2011

Comments

The full article is available from AIAA by subscription or purchase using the DOI link below.

Co-author M. Polanka has an AFRL affiliation noted on this article.  He was also an AFIT faculty member at the time of publication.

DOI

10.2514/1.45318

Source Publication

Journal of Propulsion and Power (ISSN 0748-4658 | eISSN: 1533-3876)

Recommended Citation

Lin, C.-X., Holder, R. J., Sekar, B., Zelina, J., Polanka, M. D., Thornburg, H. J., & Briones, A. M. (2011). Heat release in turbine cooling II: Numerical details of secondary combustion surrounding shaped holes. Journal of Propulsion and Power, 27(2), 269–281. https://doi.org/10.2514/1.45318