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[American Institute of Aeronautics and Astronautics 2nd AIAA Flow Control Conference - Portland, Oregon ()] 2nd AIAA Flow Control Conference - Investigations on Shock Control Bumps for Infinite Swept Wings

โœ Scribed by Kutzbach, Martin; Lutz, Thorsten; Wagner, Siegfried


Book ID
121055681
Publisher
American Institute of Aeronautics and Astronautics
Year
2004
Weight
566 KB
Category
Article
ISBN
1624100309

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