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Nozzle Geometry Effects on Corner Boundary Layers in Supersonic Wind Tunnels
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School of Engineering and Materials Science
School of Engineering and Materials Science
Nozzle Geometry Effects on Corner Boundary Layers in Supersonic Wind Tunnels
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School of Engineering and Materials Science
School of Engineering and Materials Science
Nozzle Geometry Effects on Corner Boundary Layers in Supersonic Wind Tunnels
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Nozzle Geometry Effects on Corner Boundary Layers in Supersonic Wind Tunnels
Volume
57
Pagination
1 - 4
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
DOI
10.2514/1.j058310
Journal
AIAA Journal
Issue
8
ISSN
0001-1452
Metadata
Show full item record
Authors
Sabnis, K; Babinsky, H
URI
https://qmro.qmul.ac.uk/xmlui/handle/123456789/91268
Collections
School of Engineering and Materials Science
[2927]
Copyright statements
© 2019 by K. Sabnis and H. Babinsky. Published by the American Institute of Aeronautics and Astronautics, Inc.