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Laminar Boundary Layer on a Spinning Cone at Small Angles of Attack in a Supersonic Flow

✍ Scribed by SEDNEY, R.

Book ID: 121010887
Publisher: American Institute of Aeronautics and Astronautics
Year: 1957
Weight: 776 KB
Volume: 24
Category: Article
ISSN: 1936-9956
DOI: 10.2514/8.3873

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