Comprehensive Validation of Skeletal Mechanism for Turbulent Premixed Methane–Air Flame Simulations
COMPUTATIONAL INLET SWIRL DISTORTION INVESTIGATION OF A HIGH-SPEED COMPRESSOR
NUMERICAL INVESTIGATION OF A SWIRL INDUCED FLAMELESS COMBUSTOR FOR GAS TURBINE APPLICATIONS
PROPULSION SYSTEM DESIGN FOR MARS ASCENT VEHICLES BY USING THE IN-SITU CO2
AIRCRAFT ENGINE PERFORMANCE MODEL IDENTIFICATION USING ARTIFICIAL NEURAL NETWORKS
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
STEADY-STATE CFD SIMULATIONS OF A SMALL-SCALE TURBOJET ENGINE FROM IDLE TO CRUISE CONDITIONS
MODELING OF CENTRIFUGAL COMPRESSOR PERFORMANCE USING MACHINE LEARNING TECHNIQUES
ROTOR BLADE DESIGN OPTIMIZATION FOR BOUNDARY LAYER INGESTING INLET FAN
LASER SPECIATION MEASUREMENTS DURING SHOCK TUBE IGNITION OF CYCLIC JET AND ROCKET FUEL COMPONENTS
THE REDUCTION OF CHEMICAL KINETIC MECHANISMS IN HIGH-TEMPERATURE HETEROGENEOUS FLOWS IN A NOZZLE
EXPLORATORY INVESTIGA TION OF COMBUSTION AND NVH SIGNATURE OF A DRONE JET ENGINE WITH IPK
EFFECTS OF PRESSURE ON MINIMUM HOT SURFACE IGNITION TEMPERATURES (MHSIT) IN HOT AIR CROSS-FLOWS
DESIGN OF A GEARED TURBOFAN MODULE FOR SMALL, UNMANNED AIRCRAFT APPLICATIONS
INVESTIGATION OF BUOYANCY-DRIVEN HEAT TRANSFER IN H.P COMPRESSOR DISC CAVITIES
FLOW FIELD CHARACTERIZATION OF A THIRD GENERATION SWIRL-VENTURI LEAN DIRECT INJECTOR
FLOW FIELD CHARACTERIZATION OF A THIRD GENERATION SWIRL-VENTURI LEAN DIRECT INJECTOR
NUMERICAL SIMULATION OF LEAN BLOWOUT OF ALTERNATIVE FUELS IN 7-ELEMENT LEAN DIRECT INJECTOR
NUMERICAL SIMULATION OF LEAN BLOWOUT OF ALTERNATIVE FUELS IN 7- ELEMENT LEAN DIRECT INJECTOR
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
CAPTURING AERO-PROPULSIVE COUPLING EFFECTS WITH A BODY-FORCE PROPULSOR MODEL
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