Heat transfer in a complex trailing edge passage for a high pressure turbine blade.
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Author
Contributions
- Bunker, Ronald S. - Contributor
- NASA Glenn Research Center. - Contributor
Publication
2002 - Available from NASA Center for Aerospace Information, Cleveland, Ohio, Ohio
Language
English
Word Count
0 words, Guess
Page Count
0 pages
Identifiers
- OCLC Control Number56040841
- Open LibraryOL17621431M
Alternate Titles
- Simulation results.
Subjects
Series Statement
- [NASA contractor report] -- NASA/CR-2002-211701.
- NASA contractor report -- NASA CR-211701.
Links
Other Editions
- Heat transfer in a complex trailing edge passage for a high pressure turbine blade.
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