Correction to: Aero-structural Analysis of a Scramjet Technology Demonstrator Designed to Operate at an Altitude of 23 km at Mach 5.8
Crossref DOI link: https://doi.org/10.1007/s10494-024-00569-9
Published Online: 2024-08-08
Published Print: 2024-11
Update policy: https://doi.org/10.1007/springer_crossmark_policy
de Oliveira Júnior, Paulo César
Costa Júnior, João Carlos Arantes
de Paula Toro, Paulo Gilberto
Text and Data Mining valid from 2024-08-08
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Article History
First Online: 8 August 2024
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