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Webster, Samuel Charles Leslie [Author] ; Rheinisch-Westfälische Technische Hochschule Aachen

Analysis of pressure dynamics, forced excitation and damping in a high pressure LOX/H2 combustor - [Als Manuskript gedruckt]

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Köln: DLR, Deutsches Zentrum für Luft- und Raumfahrt, [2016]

Published in: Forschungsbericht / Deutsches Zentrum für Luft- und Raumfahrt ; 2016,17
Yang, Vigor [Editor]

Liquid rocket thrust chambers : aspects of modeling, analysis, and design

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Reston, Va.: American Institute of Aeronautics and Astronautics, 2004

Published in: Progress in astronautics and aeronautics ; 200
Straub, Dieter [Author]

Thermofluiddynamics of optimized rocket propulsions : extended Lewis Code fundamentals

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Basel; Boston; Berlin: Birkhäuser, 1989
Armbruster, Wolfgang [Author] ; Rheinisch-Westfälische Technische Hochschule Aachen, Institut für Raumfahrtantriebe Hardthausen-Lampoldshausen

Untersuchung injektorgekoppelter Verbrennungsinstabilitäten in einer kryogenen Raketenbrennkammer = Investigation of injection-coupled combustion instabilities in a cryogenic rocket thrust chamber

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Köln: Deutsches Zentrum für Luft- und Raumfahrt e. V., Wissenschaftliche Information, 2022

Published in: Forschungsbericht / Deutsches Zentrum für Luft- und Raumfahrt ; 2022,09
Staudacher, Stefan [Author]

Numerische Simulation turbulenter Verbrennungsvorgänge in Raketenbrennkammern bei Einbringen flüssigen Sauerstoffs

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Berlin: Logos Berlin, 2006

Published in: Thermodynamik ; 12
Pieringer, Jutta Elfriede [Author]

Simulation selbsterregter Verbrennungsschwingungen in Raketenschubkammern im Zeitbereich

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Tonti, Federica [Author] ; Oschwald, Michael [Degree supervisor]; Jeschke, Peter [Degree supervisor]; Manfletti, Chiara [Degree supervisor]

Numerical modelling of the acoustic response of cryogenic oxygen-hydrogen rocket flames

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Aachen: Universitätsbibliothek der RWTH Aachen, 2023
Mohammadzadeh Keleshtery, Payam [Author] ; Sattelmayer, Thomas [Degree supervisor]; Oschwald, Michael [Other]; Sattelmayer, Thomas [Other]

On the Identification of Critical High-Frequency Modes and Resonator Impacts in a Gas Turbine Combustion Chamber

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München: Universitätsbibliothek der TU München, 2023
Müller, Hagen [Author] ; Pfitzner, Michael [Degree supervisor]; Hickel, Stefan [Other] Universität der Bundeswehr München, Fakultät für Luft- und Raumfahrttechnik

Simulation turbulenter nicht-vorgemischter Verbrennung bei überkritischen Drücken

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Neubiberg: Universitätsbibliothek der Universität der Bundeswehr München, 2016
Pohl, Stephanie [Author] ; Pfitzner, Michael [Degree supervisor]; Janicka, Johannes [Other] Universität der Bundeswehr München, Fakultät für Luft- und Raumfahrttechnik

Numerische Untersuchung von Verbrennungsprozessen in Raketenbrennkammern und Gasturbinen

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Neubiberg: Universitätsbibliothek der Universität der Bundeswehr München, 2016
Tonti, Federica [Author] ; Deutsches Zentrum für Luft- und Raumfahrt - Institut für Raumfahrtantriebe

Numerical Modelling of the Acoustic Response of Cryogenic Oxygen-Hydrogen Rocket Flames

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Köln: Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), Wissenschaftliche Information, 2023

Published in: Forschungsbericht ; 2023-08
Banuti, Daniel [Author]

Thermodynamic analysis and numerical modeling of supercritical injection

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Stuttgart, 2015
Bremen, Otfried Stumpf

Einfluß der Treibstoffe und der Betriebsbedingungen auf die Verbrennungs-und die Entspannungstemperatur sowie der spezifische Impuls von Raketentriebwerken unter Berücksichtigung des chemischen und des eingefrorenen Gleichgewichts

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Springer Science and Business Media LLC, 1964

Published in: Forschung im Ingenieurwesen

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