Analyse und Vergleich fertigungstechnischer Prozessketten für Flugzeugtriebwerks-Rotoren
DETERMINATION OF NITRIC OXIDE CONCENTRATIONS IN MIXTURES WITH NITROGEN TETROXIDE VIA IR SPECTROMETRY
INVESTIGATION OF COMBUSTION INSTABILITIES IN A FULL FLOW STAGED COMBUSTION MODEL ROCKET COMBUSTOR
STUDIES ON FLAME SPREAD ACCELERATION, DETONATION KERNEL IN A DUAL-THRUST ROCKET
PILOT INJECTOR REDESIGN TO REDUCE N+3 CYCLE EMISSIONS FOR A GAS-TURBINE COMBUSTOR
COMBUSTION BEHAVIOR OF AMMONIUM PERCHLORATE AT HIGH PRESSURES