The use of hot-film technique for boundary layer studies on a 21% thick airfoil
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Author
Contributions
- National Research Council of Canada. - Contributor
- National Aeronautical Establishment (Canada) - Contributor
Publication
1987 - NationalResearch Council Canada, Ottawa, Canada
Language
English
Subjects
Topics
Series Statement
- National Research Council Canada -- 27892
- Aeronautical Note / National Aeronautical Establishment -- AN45
Other Editions
- The use of hot-film technique for boundary layer studies on a 21% thick airfoil
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