Improvements in Modeling 90-degree Bleed Holes for Supersonic Inlets

Title
Improvements in Modeling 90-degree Bleed Holes for Supersonic Inlets
Authors
Keywords
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Journal
JOURNAL OF PROPULSION AND POWER
Volume 28, Issue 4, Pages 773-781
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Online
2012-06-28
DOI
10.2514/1.b34333

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