Betrachtung des Verhaltens von Bürstendichtungen unter wechselnden Betriebsbedingungen
Modellierung des nicht-linearen aerothermodynamischen Systemverhaltens von Flugantrieben
Propellants and combustion / American Institute of Aeronautics and Astronautics ; Volume 2 of 2
Propellants and combustion / American Institute of Aeronautics and Astronautics ; Volume 1 of 2
Aerodynamic design and performance of an over-wing low pressure ratio fan stage
Optical diagnostics for reacting and non-reacting flows : theory and practice
Zur Wechselwirkung zwischen Zapfluftentnahme und Hauptkanalströmung in ebenen Verdichtergittern
Untersuchung des Wärmeübergangs durch Einspritzkühlung für ein Höchstleistungsgetriebe
COMPUTATIONAL INLET SWIRL DISTORTION INVESTIGATION OF A HIGH-SPEED COMPRESSOR
NUMERICAL INVESTIGATION OF A SWIRL INDUCED FLAMELESS COMBUSTOR FOR GAS TURBINE APPLICATIONS
NUMERICAL AND EXPERIMENTAL ANALYSIS OF A SINGLE STAGE DRONE JET ENGINE
DESCRIPTION AND APPLICATION OF A SOFTWARE TOOL FOR SIMULATION OF TOMOGRAPHIC PIV DATA
DESIGN CONSIDERATIONS FOR EXTRA HIGH-PRESSURE RATIO (70) CIVIL AERO ENGINE LOW-EMISSION COMBUSTOR
EFFECTS OF DILUTION ON REACTING JET IN CROSSFLOW FLAME CHARACTERISTICS AT HIGH PRESSURE
TOWARDS IN-FLIGHT TEMPERATURE MONITORING FOR NOZZLE GUIDE VANES USING ULTRASONIC GUIDED WAVES
NUMERICAL CONTINUATION OF THE INTERACTION OF FLUTTER AND FORCED RESPONSE
INVESTIGATION OF JET GEOMETRY ON JET-IN-CROSSFLOW FLAME CHARACTERISTICS AT HIGH PRESSURE
EFFECT OF IMPURITIES IN THE RE-CYCLED CO2 STREAM ON A SUPERCRITICAL CO2 COMBUSTOR
PARAMETRIC STUDIES OF SWIRL COMBUSTOR USING LES: THE EFFECT OF INJECTORS' ANGLE
NUMERICAL INVESTIGATION OF FLOW THROUGH LABYRINTH SEALS IN GAS TURBINE ENGINES
DESIGN EXPLORATION FOR AN AXISYMMETRIC REAR BLI PROPULSOR
CAPTURING AERO-PROPULSIVE COUPLING EFFECTS WITH A BODY-FORCE PROPULSOR MODEL
DATA-DRIVEN COMBUSTION KINETIC MODELING CONCEPT OF ALTERNATIVE ALCOHOL-TO-JET (ATJ) FUEL
OPTIMAL SENSOR PLACEMENT FOR AZIMUTHAL ACOUSTIC MODE IN CYLINDRICAL DUCTS
AXIAL ROTOR DESIGN UNDER CLEAN AND DISTORTION CONDITIONS USING MEAN-LINE AND CFD METHODS