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Vibration Reduction of a Compliant Panel Under Ramp-Induced Shock Wave/Boundary Layer Interaction Through Aeroelastic Tailoring

Crossref DOI link: https://doi.org/10.1007/978-3-031-05445-7_13

Published Print: 2025-08-07

Update policy: https://doi.org/10.1007/springer_crossmark_policy

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