Early detection of thermoacoustic instabilities in a cryogenic rocket thrust chamber using combustion noise features and machine learning
- Location
-
Deutsche Nationalbibliothek Frankfurt am Main
- Extent
-
Online-Ressource
- Language
-
Englisch
- Bibliographic citation
-
In: 10.1063/5.0038817
- Event
-
Veröffentlichung
- (where)
-
Aachen
- (who)
-
Universitätsbibliothek der RWTH Aachen
- (when)
-
2021
- Creator
-
Waxenegger-Wilfing, Günther
Sengupta, Ushnish
Martin, Jan
Armbruster, Wolfgang
Hardi, Justin
Juniper, Matthew
Oschwald, Michael
- DOI
-
10.18154/RWTH-2021-08635
- URN
-
urn:nbn:de:101:1-2021091804062612022429
- Rights
-
Der Zugriff auf das Objekt ist unbeschränkt möglich.
- Last update
-
25.03.2025, 1:42 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
- Waxenegger-Wilfing, Günther
- Sengupta, Ushnish
- Martin, Jan
- Armbruster, Wolfgang
- Hardi, Justin
- Juniper, Matthew
- Oschwald, Michael
- Universitätsbibliothek der RWTH Aachen
Time of origin
- 2021
Other Objects (12)
Untersuchung injektorgekoppelter Verbrennungsinstabilitäten in einer kryogenen Raketenbrennkammer : = Investigation of injection-coupled combustion instabilities in a cryogenic rocket thrust chamber
Impact of shear-coaxial injector hydrodynamics on high-frequency combustion instabilities in a representative cryogenic rocket engine
Liquid layer combustion instabilities in paraffin-based hybrid rocket fuels
Flame-acoustic response measurements in a high-pressure, 42-injector, cryogenic rocket thrust chamber
Improved wall temperature prediction for the LUMEN rocket combustion chamber with neural networks
Improved wall temperature prediction for the lumen rocket combustion chamber with neural networks
Experimental investigation of intrinsic thermoacoustic instabilities in a combustion chamber terminated by a variable aperture
Lifetime prediction of a typical rocket combustion chamber by means of viscoplastic damage modeling
Piecewise Bilinear Characteristics of Acoustic Mode In Dual Pulse Solid Rocket Motor Combustion Chamber
Damping device to reduce the risk of injection-coupled combustion instabilities in liquid propellant rocket engines
Untersuchung selbsterregter Verbrennungsinstabilitäten in einer Raketenbrennkammer : = Investigation of self-excited combustion instabilities in a rocket combustor
Linear Stability Assessment of Cryogenic Rocket Engines
Untersuchung injektorgekoppelter Verbrennungsinstabilitäten in einer kryogenen Raketenbrennkammer : = Investigation of injection-coupled combustion instabilities in a cryogenic rocket thrust chamber
Impact of shear-coaxial injector hydrodynamics on high-frequency combustion instabilities in a representative cryogenic rocket engine
Liquid layer combustion instabilities in paraffin-based hybrid rocket fuels
Flame-acoustic response measurements in a high-pressure, 42-injector, cryogenic rocket thrust chamber
Improved wall temperature prediction for the LUMEN rocket combustion chamber with neural networks
Improved wall temperature prediction for the lumen rocket combustion chamber with neural networks
Experimental investigation of intrinsic thermoacoustic instabilities in a combustion chamber terminated by a variable aperture
Lifetime prediction of a typical rocket combustion chamber by means of viscoplastic damage modeling
Piecewise Bilinear Characteristics of Acoustic Mode In Dual Pulse Solid Rocket Motor Combustion Chamber
Damping device to reduce the risk of injection-coupled combustion instabilities in liquid propellant rocket engines
Untersuchung selbsterregter Verbrennungsinstabilitäten in einer Raketenbrennkammer : = Investigation of self-excited combustion instabilities in a rocket combustor
Linear Stability Assessment of Cryogenic Rocket Engines
Untersuchung injektorgekoppelter Verbrennungsinstabilitäten in einer kryogenen Raketenbrennkammer : = Investigation of injection-coupled combustion instabilities in a cryogenic rocket thrust chamber
Impact of shear-coaxial injector hydrodynamics on high-frequency combustion instabilities in a representative cryogenic rocket engine
Liquid layer combustion instabilities in paraffin-based hybrid rocket fuels
Flame-acoustic response measurements in a high-pressure, 42-injector, cryogenic rocket thrust chamber
Improved wall temperature prediction for the LUMEN rocket combustion chamber with neural networks
Improved wall temperature prediction for the lumen rocket combustion chamber with neural networks
Experimental investigation of intrinsic thermoacoustic instabilities in a combustion chamber terminated by a variable aperture
Lifetime prediction of a typical rocket combustion chamber by means of viscoplastic damage modeling
Piecewise Bilinear Characteristics of Acoustic Mode In Dual Pulse Solid Rocket Motor Combustion Chamber
Damping device to reduce the risk of injection-coupled combustion instabilities in liquid propellant rocket engines
Untersuchung selbsterregter Verbrennungsinstabilitäten in einer Raketenbrennkammer : = Investigation of self-excited combustion instabilities in a rocket combustor