Contribution of heat transfer to turbine blades and vanes for high temperature industrial gas turbines. Part 1: Film cooling.
- DOI
- 10.1111/j.1749-6632.2001.tb05864.x
- Published
- 2001 May
- Container
- Annals of the New York Academy of Sciences
- Publisher
- Not recorded
- Open access
- unknown
Credibility signals
limited evidence Score 43/100 under policy 1.0.0. This is a metadata assessment, not a judgment of the paper's conclusions.
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Cite this work
BibTeX
@article{allodium:10.1111/j.1749-6632.2001.tb05864.x,
title = {Contribution of heat transfer to turbine blades and vanes for high temperature industrial gas turbines. Part 1: Film cooling.},
author = {Takeishi K and Aoki S},
year = {2001},
journal = {Annals of the New York Academy of Sciences},
doi = {10.1111/j.1749-6632.2001.tb05864.x},
url = {https://doi.org/10.1111/j.1749-6632.2001.tb05864.x}
}RIS
TY - JOUR TI - Contribution of heat transfer to turbine blades and vanes for high temperature industrial gas turbines. Part 1: Film cooling. AU - Takeishi K AU - Aoki S PY - 2001 JO - Annals of the New York Academy of Sciences DO - 10.1111/j.1749-6632.2001.tb05864.x UR - https://doi.org/10.1111/j.1749-6632.2001.tb05864.x ER -
APA
K, T., & S, A. (2001). Contribution of heat transfer to turbine blades and vanes for high temperature industrial gas turbines. Part 1: Film cooling.. Annals of the New York Academy of Sciences. https://doi.org/10.1111/j.1749-6632.2001.tb05864.x
Source records
- pubmed · retrieved 2026-09-26T21:52:46.686Z