Hochschulschrift
Untersuchung injektorgekoppelter Verbrennungsinstabilitäten in einer kryogenen Raketenbrennkammer : = Investigation of injection-coupled combustion instabilities in a cryogenic rocket thrust chamber
- Weitere Titel
-
Investigation of injection-coupled combustion instabilities in a cryogenic rocket thrust chamber
- Standort
-
Deutsche Nationalbibliothek Frankfurt am Main
- Maße
-
21 cm
- Umfang
-
xxiv, 251 Seiten
- Sprache
-
Deutsch
- Anmerkungen
-
Illustrationen
Rheinisch-Westfälische Technische Hochschule Aachen, Dissertation, 2022
- Erschienen in
-
Forschungsbericht ; 2022, 09
- Klassifikation
-
Ingenieurwissenschaften und Maschinenbau
- Ereignis
-
Veröffentlichung
- (wo)
-
Köln
- (wer)
-
DLR, Deutsches Zentrum für Luft- und Raumfahrt
- (wann)
-
[2022]
- Urheber
- Inhaltsverzeichnis
- Rechteinformation
-
Bei diesem Objekt liegt nur das Inhaltsverzeichnis digital vor. Der Zugriff darauf ist unbeschränkt möglich.
- Letzte Aktualisierung
-
11.06.2025, 13:53 MESZ
Datenpartner
Dieses Objekt wird bereitgestellt von:
Deutsche Nationalbibliothek. Bei Fragen zum Objekt wenden Sie sich bitte an den Datenpartner.
Deutsche Nationalbibliothek. Bei Fragen zum Objekt wenden Sie sich bitte an den Datenpartner.
Objekttyp
- Hochschulschrift
Beteiligte
- Armbruster, Wolfgang
- DLR, Deutsches Zentrum für Luft- und Raumfahrt
Entstanden
- [2022]
Ähnliche Objekte (12)
Early detection of thermoacoustic instabilities in a cryogenic rocket thrust chamber using combustion noise features and machine learning
Flame-acoustic response measurements in a high-pressure, 42-injector, cryogenic rocket thrust chamber
Measuring the velocity field of a shear-coaxial, cryogenic flame in a high-pressure rocket thrust chamber
Impact of shear-coaxial injector hydrodynamics on high-frequency combustion instabilities in a representative cryogenic rocket engine
Experimentelle Untersuchung der laserinduzierten Zündung von kryogenen Flüssigkeitsraketenbrennkammern : = Experimental investigation of the laser-induced ignition of cryogenic liquid rocket combustors
Linear Stability Assessment of Cryogenic Rocket Engines
ADCS Design for a Sounding Rocket with Thrust Vectoring
Numerical modelling of the acoustic response of cryogenic oxygen-haydrogen rocket flames : = Numerische Modellierung der akustischen Antwort von kryogenen Wasserstoff-Sauerstoff-Raketenflammen
Liquid layer combustion instabilities in paraffin-based hybrid rocket fuels
Variations and Control of Thrust and Mixture Ratio in Hybrid Rocket Motors
Numerical modelling of the acoustic response of cryogenic oxygen-hydrogen rocket flames
Numerical Modelling of the Acoustic Response of Cryogenic Oxygen-Hydrogen Rocket Flames
Early detection of thermoacoustic instabilities in a cryogenic rocket thrust chamber using combustion noise features and machine learning
Flame-acoustic response measurements in a high-pressure, 42-injector, cryogenic rocket thrust chamber
Measuring the velocity field of a shear-coaxial, cryogenic flame in a high-pressure rocket thrust chamber
Impact of shear-coaxial injector hydrodynamics on high-frequency combustion instabilities in a representative cryogenic rocket engine
Experimentelle Untersuchung der laserinduzierten Zündung von kryogenen Flüssigkeitsraketenbrennkammern : = Experimental investigation of the laser-induced ignition of cryogenic liquid rocket combustors
Linear Stability Assessment of Cryogenic Rocket Engines
ADCS Design for a Sounding Rocket with Thrust Vectoring
Numerical modelling of the acoustic response of cryogenic oxygen-haydrogen rocket flames : = Numerische Modellierung der akustischen Antwort von kryogenen Wasserstoff-Sauerstoff-Raketenflammen
Liquid layer combustion instabilities in paraffin-based hybrid rocket fuels
Variations and Control of Thrust and Mixture Ratio in Hybrid Rocket Motors
Numerical modelling of the acoustic response of cryogenic oxygen-hydrogen rocket flames
Numerical Modelling of the Acoustic Response of Cryogenic Oxygen-Hydrogen Rocket Flames
Early detection of thermoacoustic instabilities in a cryogenic rocket thrust chamber using combustion noise features and machine learning
Flame-acoustic response measurements in a high-pressure, 42-injector, cryogenic rocket thrust chamber
Measuring the velocity field of a shear-coaxial, cryogenic flame in a high-pressure rocket thrust chamber
Impact of shear-coaxial injector hydrodynamics on high-frequency combustion instabilities in a representative cryogenic rocket engine
Experimentelle Untersuchung der laserinduzierten Zündung von kryogenen Flüssigkeitsraketenbrennkammern : = Experimental investigation of the laser-induced ignition of cryogenic liquid rocket combustors
Linear Stability Assessment of Cryogenic Rocket Engines
ADCS Design for a Sounding Rocket with Thrust Vectoring
Numerical modelling of the acoustic response of cryogenic oxygen-haydrogen rocket flames : = Numerische Modellierung der akustischen Antwort von kryogenen Wasserstoff-Sauerstoff-Raketenflammen
Liquid layer combustion instabilities in paraffin-based hybrid rocket fuels
Variations and Control of Thrust and Mixture Ratio in Hybrid Rocket Motors
Numerical modelling of the acoustic response of cryogenic oxygen-hydrogen rocket flames