Hochschulschrift
Liquid layer combustion instabilities in paraffin-based hybrid rocket fuels
- Location
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Deutsche Nationalbibliothek Frankfurt am Main
- Dimensions
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21 cm
- Extent
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xx, 180 Seiten
- Edition
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Als Manusktript gedruckt
- Language
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Englisch
- Notes
-
Illustrationen
University Stuttgart, Dissertation, 2020
- Bibliographic citation
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Forschungsbericht ; 2020, 38
- Classification
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Ingenieurwissenschaften und Maschinenbau
Technische Chemie
- Event
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Veröffentlichung
- (where)
-
Köln
- (who)
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DLR, Deutsches Zentrum für Luft- und Raumfahrt
- (when)
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[2020]
- Creator
- Table of contents
- Rights
-
Bei diesem Objekt liegt nur das Inhaltsverzeichnis digital vor. Der Zugriff darauf ist unbeschränkt möglich.
- Last update
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11.06.2025, 1:43 PM 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.
Object type
- Hochschulschrift
Associated
- Petrarolo, Anna
- DLR, Deutsches Zentrum für Luft- und Raumfahrt
Time of origin
- [2020]
Other Objects (12)
Combustion phenomena of advanced hybrid rocket fuels
Understanding Kelvin–Helmholtz instability in paraffin-based hybrid rocket fuels
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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
Impact of shear-coaxial injector hydrodynamics on high-frequency combustion instabilities in a representative cryogenic rocket engine
Early detection of thermoacoustic instabilities in a cryogenic rocket thrust chamber using combustion noise features and machine learning
Turbulent Combustion Phenomena in Methane Rocket Engines
Untersuchung injektorgekoppelter Verbrennungsinstabilitäten in einer kryogenen Raketenbrennkammer : = Investigation of injection-coupled combustion instabilities in a cryogenic rocket thrust chamber
Handbook of combustion, Vol. 4.. Solid fuels
Control authority for active damping of combustion instabilities
Combustion phenomena of advanced hybrid rocket fuels
Understanding Kelvin–Helmholtz instability in paraffin-based hybrid rocket fuels
Synthetic fuels and combustion
Combustion of peroxy-fuels
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
Impact of shear-coaxial injector hydrodynamics on high-frequency combustion instabilities in a representative cryogenic rocket engine
Early detection of thermoacoustic instabilities in a cryogenic rocket thrust chamber using combustion noise features and machine learning
Turbulent Combustion Phenomena in Methane Rocket Engines
Untersuchung injektorgekoppelter Verbrennungsinstabilitäten in einer kryogenen Raketenbrennkammer : = Investigation of injection-coupled combustion instabilities in a cryogenic rocket thrust chamber
Handbook of combustion, Vol. 4.. Solid fuels
Control authority for active damping of combustion instabilities
Combustion phenomena of advanced hybrid rocket fuels
Understanding Kelvin–Helmholtz instability in paraffin-based hybrid rocket fuels
Synthetic fuels and combustion
Combustion of peroxy-fuels
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
Impact of shear-coaxial injector hydrodynamics on high-frequency combustion instabilities in a representative cryogenic rocket engine
Early detection of thermoacoustic instabilities in a cryogenic rocket thrust chamber using combustion noise features and machine learning
Turbulent Combustion Phenomena in Methane Rocket Engines
Untersuchung injektorgekoppelter Verbrennungsinstabilitäten in einer kryogenen Raketenbrennkammer : = Investigation of injection-coupled combustion instabilities in a cryogenic rocket thrust chamber
Handbook of combustion, Vol. 4.. Solid fuels