Future Space-Transport-System Components under High Thermal and Mechanical Loads
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Future Space-Transport-System Components under High Thermal and Mechanical Loads
Results from the DFG Collaborative Research Center TRR40
Schroeder, Wolfgang; Adams, Nikolaus A.; Sattelmayer, Thomas; Radespiel, Rolf; Stemmer, Christian; Weigand, Bernhard; Haidn, Oskar J.
Springer Nature Switzerland AG
10/2021
419
Mole
Inglês
9783030538491
15 a 20 dias
658
Descrição não disponível.
Collaborative Research for Future Space Transportation Systems.- Innovative Cooling for Rocket Combustion Chambers.- Film Cooling in Rocket Nozzle.- Heat Transfer in Pulsating Flow and its Impact on Temperature Distribution and Damping Performance of Acoustic Resonators.- E?ects of a Launcher's External Fow on a Dual-Bell Nozzle Flow.- Interaction of Wake and Propulsive Jet Flow of a Generic Space Launcher.- Numerical Analysis of the Turbulent Wake for a Generic Space Launcher with a Dual-Bell Nozzle.
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Rocket Propulsion;Multi-scale Modelling in Aerospace;Real-gas Thermodynamics;Multi-phase Flow Simulation;Compressible Shear-layer;Turbulent Heat Flux Model;LOX/CH4 Combustor;Multi-element Combustor Chamber;Wall Heat Transfer Prediction;SFB/TRR40;Open Access
Collaborative Research for Future Space Transportation Systems.- Innovative Cooling for Rocket Combustion Chambers.- Film Cooling in Rocket Nozzle.- Heat Transfer in Pulsating Flow and its Impact on Temperature Distribution and Damping Performance of Acoustic Resonators.- E?ects of a Launcher's External Fow on a Dual-Bell Nozzle Flow.- Interaction of Wake and Propulsive Jet Flow of a Generic Space Launcher.- Numerical Analysis of the Turbulent Wake for a Generic Space Launcher with a Dual-Bell Nozzle.
Este título pertence ao(s) assunto(s) indicados(s). Para ver outros títulos clique no assunto desejado.
