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
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
EXPLORATION OF THE VERSATILE ELECTRICALLY AUGMENTED TURBINE ENGINE GEARBOX CONCEPT
THE AERODYNAMICS OF CIRCUMFERENTIAL CASING-GROOVE IN A TRANSONIC COMPRESSOR
REDUCED-ORDER MODELING OF AEROELASTICITY IN EXTREME SPEED TURBOCHARGERS
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
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
APPLICATION OF A COMPACT COMBUSTOR IN SMALL-SCALE JETCAT ENGINES
EFFECT OF VARIABLE INLET GUIDE VANES (VIGV) ON A SMALL GAS TURBINE ENGINE
DESIGN AND CHARACTERIZATION OF THE DUAL INDEPENDENT SWIRL COMBUSTOR FACILITY (DISCO)
DEFINING A TESTBED FOR THE U.S. TURBINE INDUSTRY: THE NATIONAL EXPERIMENTAL TURBINE (NEXT)
MULTIDISCIPLINARY OPTIMIZATION OF A HELICOPTER GTE TURBINE
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