Boundary-Layer Development Downstream of Normal Shock in Transonic Intakes at Incidence

Published 2019 View Full Article

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Title
Boundary-Layer Development Downstream of Normal Shock in Transonic Intakes at Incidence
Authors
Keywords
-
Journal
AIAA JOURNAL
Volume -, Issue -, Pages 1-11
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Online
2019-08-16
DOI
10.2514/1.j058508
References
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