Correction to: Aero-structural Analysis of a Scramjet Technology Demonstrator Designed to Operate at an Altitude of 23 km at Mach 5.8

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Bibliographische Detailangaben
Veröffentlicht in:	Flow, turbulence and combustion turbulence and combustion, 2024, Vol.113 (4), p.1053-1053
Hauptverfasser:	de Oliveira Júnior, Paulo César, Costa Júnior, João Carlos Arantes, de Paula Toro, Paulo Gilberto
Format:	Artikel
Sprache:	eng
Schlagworte:	Automotive Engineering Correction Engineering Engineering Fluid Dynamics Engineering Thermodynamics Fluid- and Aerodynamics Heat and Mass Transfer Structural analysis Supersonic combustion ramjet engines Technology assessment Technology demonstrator
Online-Zugang:	Volltext
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