Flame-acoustic response measurements in a high-pressure, 42-injector, cryogenic rocket thrust chamber
- Location
-
Deutsche Nationalbibliothek Frankfurt am Main
- Extent
-
Online-Ressource
- Language
-
Englisch
- Bibliographic citation
-
In: 10.1016/j.proci.2020.05.020
- Event
-
Veröffentlichung
- (where)
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Aachen
- (who)
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Universitätsbibliothek der RWTH Aachen
- (when)
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2020
- Creator
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Armbruster, Wolfgang
Hardi, Justin S.
Oschwald, Michael
- DOI
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10.18154/RWTH-2021-04796
- URN
-
urn:nbn:de:101:1-2021052203313472724145
- Rights
-
Der Zugriff auf das Objekt ist unbeschränkt möglich.
- Last update
-
25.03.2025, 1:44 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
- Armbruster, Wolfgang
- Hardi, Justin S.
- Oschwald, Michael
- Universitätsbibliothek der RWTH Aachen
Time of origin
- 2020
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Linear Stability Assessment of Cryogenic Rocket Engines
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Untersuchung injektorgekoppelter Verbrennungsinstabilitäten in einer kryogenen Raketenbrennkammer : = Investigation of injection-coupled combustion instabilities in a cryogenic rocket thrust chamber
Testing the limits of the cryogenic nucleation pulse chamber
Numerical modelling of the acoustic response of cryogenic oxygen-hydrogen rocket flames
Numerical Modelling of the Acoustic Response of Cryogenic Oxygen-Hydrogen Rocket Flames
Experimental Investigation of Flame Anchoring Behavior in a LOX/LNG Rocket Combustor
Simulation and modeling of droplet formation in flash atomization of cryogenic rocket propellants
Simulation of the sloshing behaviour of two-phase flows in cryogenic rocket upper stages
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Measuring the velocity field of a shear-coaxial, cryogenic flame in a high-pressure rocket thrust chamber
Flame Characteristics and Response of a High-Pressure LOX/CNG Rocket Combustor with Large Optical Access
Linear Stability Assessment of Cryogenic Rocket Engines
Early detection of thermoacoustic instabilities in a cryogenic rocket thrust chamber using combustion noise features and machine learning
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Testing the limits of the cryogenic nucleation pulse chamber
Numerical modelling of the acoustic response of cryogenic oxygen-hydrogen rocket flames
Numerical Modelling of the Acoustic Response of Cryogenic Oxygen-Hydrogen Rocket Flames
Experimental Investigation of Flame Anchoring Behavior in a LOX/LNG Rocket Combustor
Simulation and modeling of droplet formation in flash atomization of cryogenic rocket propellants
Simulation of the sloshing behaviour of two-phase flows in cryogenic rocket upper stages