Acoustic modes in a plenum downstream of a multitube pulse detonation combustor
- Location
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Deutsche Nationalbibliothek Frankfurt am Main
- Extent
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Online-Ressource
- Language
-
Englisch
- Bibliographic citation
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In: AIAA Journal (59:11) - Reston, Va. [u.a.] : American Institute of Aeronautics and Astronautics - S. 4569-4580
- Event
-
Veröffentlichung
- (where)
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Berlin
- (who)
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Technische Universität Berlin
- (when)
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2022
- Creator
-
Habicht, Fabian
Yücel, Fatma Cansu
Haghdoost, Mohammad Rezay
Oberleithner, Kilian
Paschereit, Christian Oliver
- DOI
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10.14279/depositonce-15714
- Handle
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11303/16935
- URN
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urn:nbn:de:101:1-2022051802053093795094
- Rights
-
Der Zugriff auf das Objekt ist unbeschränkt möglich.
- Last update
-
25.03.2025, 1:52 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
- Habicht, Fabian
- Yücel, Fatma Cansu
- Haghdoost, Mohammad Rezay
- Oberleithner, Kilian
- Paschereit, Christian Oliver
- Technische Universität Berlin
Time of origin
- 2022
Other Objects (12)
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Aerodynamic investigation of guide vane configurations downstream a rotating detonation combustor
Pulse detonation exhaust and methods for damping its transient characteristic
Reduction in the run-up distance for the deflagration-to-detonation transition and applications to pulse detonation combustion
Towards the implementation of a pulse detonation combustor into a gas turbine
Detonation
VI. Detonationen.
Stehende Detonationen
Toward detonation theory
Detonation of condensed explosives
Downstream processing
Detonation initiation by shock focusing at elevated pressure conditions in a pulse detonation combustor
Unsteady Effects on NOx Measurements in Pulse Detonation Combustion
Aerodynamic investigation of guide vane configurations downstream a rotating detonation combustor
Pulse detonation exhaust and methods for damping its transient characteristic
Reduction in the run-up distance for the deflagration-to-detonation transition and applications to pulse detonation combustion
Towards the implementation of a pulse detonation combustor into a gas turbine
Detonation
VI. Detonationen.
Stehende Detonationen
Toward detonation theory
Detonation of condensed explosives
Downstream processing
Detonation initiation by shock focusing at elevated pressure conditions in a pulse detonation combustor
Unsteady Effects on NOx Measurements in Pulse Detonation Combustion
Aerodynamic investigation of guide vane configurations downstream a rotating detonation combustor
Pulse detonation exhaust and methods for damping its transient characteristic
Reduction in the run-up distance for the deflagration-to-detonation transition and applications to pulse detonation combustion
Towards the implementation of a pulse detonation combustor into a gas turbine
Detonation
VI. Detonationen.
Stehende Detonationen
Toward detonation theory
Detonation of condensed explosives