Transpiration cooling of a turbulent boundary layer in an axisymmetric nozzle
- 1 April 1964
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 2 (4), 617-624
- https://doi.org/10.2514/3.2397
Abstract
No abstract availableKeywords
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- Technical NotesJournal of Jet Propulsion, 1957