Betrachtung des Verhaltens von Bürstendichtungen unter wechselnden Betriebsbedingungen
Betrachtung des Verhaltens von Bürstendichtungen unter wechselnden Betriebsbedingungen
Modellierung des nicht-linearen aerothermodynamischen Systemverhaltens von Flugantrieben
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
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
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
LASER INDUCED SPARK IGNITION FOR LAMINAR PREMIXED HYDROGEN AIR JETS
INVESTIGATION OF ELEVATED TURBULENCE ON HIGH-LIFT LOW PRESSURE TURBINE ENDWALL FLOWS
UTILIZING ELECTRICAL POWER EXTRACTION FOR STABILITY BLEED REDUCTION WITHIN GAS TURBINE ENGINES
AN INVESTIGATION OF COOLED COOLING AIR FOR A MACH 2.2 COMMERCIAL SUPERSONIC TRANSPORT
THRUST MEASUREMENTS USING ACOUSTIC SENSING ON A TURBOFAN ENGINE EXHAUST PLUME
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
CO2 SENSITIZED PROPANE OXIDATION AT 100 ATM IN A NOVEL JET STIRRED REACTOR
SIMULATION OF REACTING JET IN VITIATED CROSSFLOW AT 5 ATMOSPHERES USING ADAPTIVE MESH REFINEMENT
A ROBUST INITIALIZATION APPROACH OF MULTI-POINT SYNTHESIS SCHEMES FOR AERO-ENGINE CONCEPTUAL DESIGN
NUMERICAL SIMULATION ON THE EFFECTS OF HYDROGEN DOPING IN NATURAL GAS JET-IN-CROSSFLOW COMBUSTION