Hochschulschrift
Radiation from High Pressure Hydrogen-Oxygen Flames and its Use in Assessing Rocket Combustion Instability
- Weitere Titel
-
Strahlung von Hochdruck Wasserstoff-Sauerstoff Flammen und ihr Nutzen zur Beurteilung von Verbrennungsinstabilitäten in Raketenbrennkammern
- Standort
-
Deutsche Nationalbibliothek Frankfurt am Main
- Umfang
-
Online-Ressource
- Sprache
-
Englisch
- Anmerkungen
-
München, Technische Universität München, Diss., 2015
- Schlagwort
-
Flüssigkeitsraketentriebwerk
Raketentreibstoff
Hydroxyl
Flamme
Laminare Strömung
Strahlungsmessung
Instabilität
Verbrennung
- Ereignis
-
Veröffentlichung
- (wo)
-
München
- (wer)
-
Universitätsbibliothek der TU München
- (wann)
-
2015
- Urheber
-
Fiala, Thomas
- Beteiligte Personen und Organisationen
-
Sattelmayer, Thomas
Oschwald, Michael
- URN
-
urn:nbn:de:bvb:91-diss-20150720-1243479-1-5
- Rechteinformation
-
Der Zugriff auf das Objekt ist unbeschränkt möglich.
- Letzte Aktualisierung
-
14.08.2025, 11:04 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
- Sattelmayer, Thomas
- Oschwald, Michael
- Universitätsbibliothek der TU München
Entstanden
- 2015
Ähnliche Objekte (12)
Analysis and Improvement of Rocket Engine Combustion Stability Simulations
Linear Stability Assessment of Cryogenic Rocket Engines
Determination of the Heat Release Distribution in Turbulent Flames by Chemiluminescence Imaging
Heat Transfer Predictions in Hydrogen/Oxygen and Methane/Oxygen Rocket Engines
Numerical Investigation of Combustion Characteristics in GO2/GCH4 Combustors with Reaction Mechanisms
Combustion Noise Prediction with Linearized Navier-Stokes Equations and Spectral Sound Sources
Numerical Modelling of Boundary Layer Flashback in Premixed Hydrogen-Air Combustion Systems
On the Formation of Nitrogen Oxides During the Combustion of Partially Pre-Vaporized Droplets
Combustion Model for the Computation of Flame Propagation in Lean Hydrogen-Air Mixtures at Low Turbulence
Boundary Layer Flashback in Premixed Combustion Systems
Design and Experimental Study of Injection Systems in a Supersonic Combustion Chamber
On the Chemical Effect of Steam Addition to Premixed Hydrogen Flames with Respect to $$\text NO}_\text x}$$ NO x Emissions and Flame Speed
Analysis and Improvement of Rocket Engine Combustion Stability Simulations
Linear Stability Assessment of Cryogenic Rocket Engines
Determination of the Heat Release Distribution in Turbulent Flames by Chemiluminescence Imaging
Heat Transfer Predictions in Hydrogen/Oxygen and Methane/Oxygen Rocket Engines
Numerical Investigation of Combustion Characteristics in GO2/GCH4 Combustors with Reaction Mechanisms
Combustion Noise Prediction with Linearized Navier-Stokes Equations and Spectral Sound Sources
Numerical Modelling of Boundary Layer Flashback in Premixed Hydrogen-Air Combustion Systems
On the Formation of Nitrogen Oxides During the Combustion of Partially Pre-Vaporized Droplets
Combustion Model for the Computation of Flame Propagation in Lean Hydrogen-Air Mixtures at Low Turbulence
Boundary Layer Flashback in Premixed Combustion Systems
Design and Experimental Study of Injection Systems in a Supersonic Combustion Chamber
On the Chemical Effect of Steam Addition to Premixed Hydrogen Flames with Respect to $$\text NO}_\text x}$$ NO x Emissions and Flame Speed
Analysis and Improvement of Rocket Engine Combustion Stability Simulations
Linear Stability Assessment of Cryogenic Rocket Engines
Determination of the Heat Release Distribution in Turbulent Flames by Chemiluminescence Imaging
Heat Transfer Predictions in Hydrogen/Oxygen and Methane/Oxygen Rocket Engines
Numerical Investigation of Combustion Characteristics in GO2/GCH4 Combustors with Reaction Mechanisms
Combustion Noise Prediction with Linearized Navier-Stokes Equations and Spectral Sound Sources
Numerical Modelling of Boundary Layer Flashback in Premixed Hydrogen-Air Combustion Systems
On the Formation of Nitrogen Oxides During the Combustion of Partially Pre-Vaporized Droplets
Combustion Model for the Computation of Flame Propagation in Lean Hydrogen-Air Mixtures at Low Turbulence
Boundary Layer Flashback in Premixed Combustion Systems
Design and Experimental Study of Injection Systems in a Supersonic Combustion Chamber