Numerical Modelling of the Acoustic Response of Cryogenic Oxygen-Hydrogen Rocket Flames
- Location
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Deutsche Nationalbibliothek Frankfurt am Main
- ISSN
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1434-8454
- Extent
-
Online-Ressource
- Language
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Englisch
- Notes
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Aachen, Rheinisch-Westfälische Technische Hochschule Aachen (RWTH), Dissertation, 2023
- Bibliographic citation
-
Forschungsbericht ; 2023-08
- Keyword
-
Numerische Strömungssimulation
Verbrennung
Raketentriebwerk
Instabilität
Brennkammer
Flamme
- Event
-
Veröffentlichung
- (where)
-
Köln
- (who)
-
Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), Wissenschaftliche Information
- (when)
-
2023
- Creator
- Contributor
-
Deutsches Zentrum für Luft- und Raumfahrt - Institut für Raumfahrtantriebe
- DOI
-
10.57676/ns5k-2t91
- URN
-
urn:nbn:de:101:1-2023082209050880513795
- Rights
-
Der Zugriff auf das Objekt ist unbeschränkt möglich.
- Last update
-
25.03.2025, 1:48 PM CET
Data provider
This object is provided by:
Deutsche Nationalbibliothek. If you have any questions about the object, please contact the data provider.
Deutsche Nationalbibliothek. If you have any questions about the object, please contact the data provider.
Associated
- Tonti, Federica
- Deutsches Zentrum für Luft- und Raumfahrt - Institut für Raumfahrtantriebe
- Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), Wissenschaftliche Information
Time of origin
- 2023
Other Objects (12)
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Numerical modelling of the acoustic response of cryogenic oxygen-hydrogen rocket flames
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Flame-acoustic response measurements in a high-pressure, 42-injector, cryogenic rocket thrust chamber
Radiation from High Pressure Hydrogen-Oxygen Flames and its Use in Assessing Rocket Combustion Instability
Radiation from high pressure hydrogen-oxygen flames and its use in assessing rocket combustion instability
Linear Stability Assessment of Cryogenic Rocket Engines
The oxycoal process with cryogenic oxygen supply
Experimental and numerical study of transcritical oxygen-hydrogen rocket flame response to transverse acoustic excitation
Heat Transfer Predictions in Hydrogen/Oxygen and Methane/Oxygen Rocket Engines
Computation of the thermoacoustic driving capability of rocket engine flames with detailed chemistry
Modeling and simulation of charged species in lean methane-oxygen flames
Measurement and scaling of acoustic transfer matrices of premixed swirl flames
Numerical modelling of the acoustic response of cryogenic oxygen-hydrogen rocket flames
Numerical modelling of the acoustic response of cryogenic oxygen-haydrogen rocket flames : = Numerische Modellierung der akustischen Antwort von kryogenen Wasserstoff-Sauerstoff-Raketenflammen
Flame-acoustic response measurements in a high-pressure, 42-injector, cryogenic rocket thrust chamber
Radiation from High Pressure Hydrogen-Oxygen Flames and its Use in Assessing Rocket Combustion Instability
Radiation from high pressure hydrogen-oxygen flames and its use in assessing rocket combustion instability
Linear Stability Assessment of Cryogenic Rocket Engines
The oxycoal process with cryogenic oxygen supply
Experimental and numerical study of transcritical oxygen-hydrogen rocket flame response to transverse acoustic excitation
Heat Transfer Predictions in Hydrogen/Oxygen and Methane/Oxygen Rocket Engines
Computation of the thermoacoustic driving capability of rocket engine flames with detailed chemistry
Modeling and simulation of charged species in lean methane-oxygen flames