Hochschulschrift
Radiation from high pressure hydrogen-oxygen flames and its use in assessing rocket combustion instability
- Standort
-
Deutsche Nationalbibliothek Frankfurt am Main
- ISBN
-
9783843922500
3843922500
- Maße
-
21 cm, 238 g
- Umfang
-
xv, 135 Seiten
- Ausgabe
-
1. Auflage
- Sprache
-
Englisch
- Anmerkungen
-
Illustrationen, Diagramme
Technische Universität München, Dissertation, 2015
- Schlagwort
-
Flüssigkeitsraketentriebwerk
Raketentreibstoff
Hydroxyl
Flamme
Laminare Strömung
Strahlungsmessung
Instabilität
Verbrennung
- Ereignis
-
Veröffentlichung
- (wo)
-
München
- (wer)
-
Verlag Dr. Hut
- (wann)
-
2015
- Urheber
-
Fiala, Thomas
- Beteiligte Personen und Organisationen
- Inhaltsverzeichnis
- Rechteinformation
-
Bei diesem Objekt liegt nur das Inhaltsverzeichnis digital vor. Der Zugriff darauf ist unbeschränkt möglich.
- Letzte Aktualisierung
-
11.06.2025, 14:20 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
- Fiala, Thomas
- Verlag Dr. Hut. München
- Verlag Dr. Hut
Entstanden
- 2015
Ähnliche Objekte (12)
Computation of the thermoacoustic driving capability of rocket engine flames with detailed chemistry
Experimental investigation and spectral modeling of turbulent combustion noise from premixed and non-premixed flames
Investigation on heat transfer and injector design criteria for methane-oxygen rocket combustion chambers
Pollutant formation in premixed natural gas swirl flames with water injection
Analysis and low-order modeling of interactions between acoustics, hydrodynamics and premixed flames
Numerically efficient hybrid RANS-LES of supersonic combustion
Radiation from High Pressure Hydrogen-Oxygen Flames and its Use in Assessing Rocket Combustion Instability
Influence of the injector geometry on mixing and lift-off of premixed jet flames in hot cross flow
Investigation on heat transfer in single- and multi-element GOX-GCH4 model rocket engines
Modeling and analysis of high-frequency thermoacoustic oscillations in gas turbine combustion chambers
Fly ash formation and deposition during pulverized fuel combustion : numerical and experimental investigations
Auto-ignition and combustion of fuel jets in vitiated co-flow at elevated pressure
Computation of the thermoacoustic driving capability of rocket engine flames with detailed chemistry
Experimental investigation and spectral modeling of turbulent combustion noise from premixed and non-premixed flames
Investigation on heat transfer and injector design criteria for methane-oxygen rocket combustion chambers
Pollutant formation in premixed natural gas swirl flames with water injection
Analysis and low-order modeling of interactions between acoustics, hydrodynamics and premixed flames
Numerically efficient hybrid RANS-LES of supersonic combustion
Radiation from High Pressure Hydrogen-Oxygen Flames and its Use in Assessing Rocket Combustion Instability
Influence of the injector geometry on mixing and lift-off of premixed jet flames in hot cross flow
Investigation on heat transfer in single- and multi-element GOX-GCH4 model rocket engines
Modeling and analysis of high-frequency thermoacoustic oscillations in gas turbine combustion chambers
Fly ash formation and deposition during pulverized fuel combustion : numerical and experimental investigations
Auto-ignition and combustion of fuel jets in vitiated co-flow at elevated pressure
Computation of the thermoacoustic driving capability of rocket engine flames with detailed chemistry
Experimental investigation and spectral modeling of turbulent combustion noise from premixed and non-premixed flames
Investigation on heat transfer and injector design criteria for methane-oxygen rocket combustion chambers
Pollutant formation in premixed natural gas swirl flames with water injection
Analysis and low-order modeling of interactions between acoustics, hydrodynamics and premixed flames
Numerically efficient hybrid RANS-LES of supersonic combustion
Radiation from High Pressure Hydrogen-Oxygen Flames and its Use in Assessing Rocket Combustion Instability
Influence of the injector geometry on mixing and lift-off of premixed jet flames in hot cross flow
Investigation on heat transfer in single- and multi-element GOX-GCH4 model rocket engines
Modeling and analysis of high-frequency thermoacoustic oscillations in gas turbine combustion chambers
Fly ash formation and deposition during pulverized fuel combustion : numerical and experimental investigations