Aerodynamic characteristics of the retro propulsion landing burn of vertically landing launchers

In the frame of the European funded H2020 project RETALT (retro propulsion-assisted landing technologies), the unsteady aerodynamics of vertically descending and landing launchers have been investigated. In this paper, experimental data of the landing burn tested in the Vertical Free-Jet Facility Co...

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Veröffentlicht in:	Experiments in fluids 2024-08, Vol.65 (8), Article 115
Hauptverfasser:	Marwege, Ansgar, Gülhan, Ali
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamic characteristics Cold gas Engineering Engineering Fluid Dynamics Engineering Thermodynamics Fluid- and Aerodynamics Gas jets Heat and Mass Transfer Landing Launchers Pressure ratio Proper Orthogonal Decomposition Propulsion Research Article Scale (ratio) Steady flow Strouhal number Subsonic aircraft Unsteady aerodynamics Unsteady flow Wind tunnel testing Wind tunnels
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