Impact of shear-coaxial injector hydrodynamics on high-frequency combustion instabilities in a representative cryogenic rocket engine
- Location
-
Deutsche Nationalbibliothek Frankfurt am Main
- Extent
-
Online-Ressource
- Language
-
Englisch
- Bibliographic citation
-
In: 10.1177/17568277221093848
- Classification
-
Ingenieurwissenschaften und Maschinenbau
- Event
-
Veröffentlichung
- (where)
-
Aachen
- (who)
-
Universitätsbibliothek der RWTH Aachen
- (when)
-
2022
- Creator
-
Armbruster, Wolfgang
Hardi, Justin
Oschwald, Michael
- DOI
-
10.18154/RWTH-2022-06597
- URN
-
urn:nbn:de:101:1-2022070403321608438199
- Rights
-
Der Zugriff auf das Objekt ist unbeschränkt möglich.
- Last update
-
15.08.2025, 7:30 AM CEST
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
- Oschwald, Michael
- Universitätsbibliothek der RWTH Aachen
Time of origin
- 2022
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Flame-acoustic response measurements in a high-pressure, 42-injector, cryogenic rocket thrust chamber
Low-order modeling approach for the prediction of transverse combustion instabilities in multi-injector engines
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SCHICK EVERSHARP INJECTOR RAZOR
On coaxial circles.
Co-axial monodromy
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Hydrodynamics and instabilities of relativistic superfluids at finite superflow
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Injector-coupled thermoacoustic instabilities in an experimental LOX-methane rocket combustor during start-up
Characterizing the attenuation of coaxial and rectangular microwave-frequency waveguides at cryogenic temperatures
Flame-acoustic response measurements in a high-pressure, 42-injector, cryogenic rocket thrust chamber
Low-order modeling approach for the prediction of transverse combustion instabilities in multi-injector engines
Measuring the velocity field of a shear-coaxial, cryogenic flame in a high-pressure rocket thrust chamber
Capabilities and limitations of smoothed particle hydrodynamics for the simulation of two‐phase flow instabilities
SCHICK EVERSHARP INJECTOR RAZOR
On coaxial circles.
Co-axial monodromy
On coaxial circles.
Hydrodynamics and instabilities of relativistic superfluids at finite superflow
Injector-coupled thermoacoustic instabilities in an experimental LOX-methane rocket combustor during start-up
Injector-coupled thermoacoustic instabilities in an experimental LOX-methane rocket combustor during start-up
Characterizing the attenuation of coaxial and rectangular microwave-frequency waveguides at cryogenic temperatures
Flame-acoustic response measurements in a high-pressure, 42-injector, cryogenic rocket thrust chamber
Low-order modeling approach for the prediction of transverse combustion instabilities in multi-injector engines
Measuring the velocity field of a shear-coaxial, cryogenic flame in a high-pressure rocket thrust chamber
Capabilities and limitations of smoothed particle hydrodynamics for the simulation of two‐phase flow instabilities
SCHICK EVERSHARP INJECTOR RAZOR
On coaxial circles.
Co-axial monodromy