Neuartiger Wasserstoffinjektor zur Flammenstabilisierung in einer Überschallströmung
Seminar des Sonderforschungsbereichs 255
TU München, Munich, Germany
2002
Application of Spontaneous Raman Scattering to the Flowfield in a Scramjet Combustor
Proceedings of the 11th International Conference on Methods of Aerophysical Research
Novosibirsk-Denisova Cave, Russia
2002
Stabilitätsanalyse der Verbrennung in Gasturbinen unter Anwendung von modalen Ansätzen und Finite-Element-Methoden
Berechnungsverfahren für Brennkammerströmung in Raketen- und Gasturbinennbrenkammern
2002
Study of the Bubble Characteristics and the Local Void Fraction in Subcooled Flow Boiling Using Digital Imaging- and Analysing Techniques
Journal of Experimental Thermal and Fluid Science
2002
26
147-155
Novel Two Stage Injector for Hydrogen Flame Stabilization in Supersonic Airflow
AIAA/AAAF 11th International Space Planes and Hypersonic Systems and Technologies Conference
2002
Numerical Investigation of Fuel Mixing, Ignition and Flame Stabilization by a Strut Injector in a Scramjet Combustor
Proceedings of the 11th International Conference on Methods of Aerophysical Research
2002
Einfluss des Vorheizerausbrands auf die Flammenstabilisierung in einer Überschallbrennkammer
Seminar des Sonderforschungsbereichs 255
2002
Processing and analysis of holographic images for the bubbles characterisation in an aerated stirred vessel
Proceedings of Eurotherm 71
2002