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
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
NUMERICAL SIMULATION OF LEAN BLOWOUT OF ALTERNATIVE FUELS IN 7-ELEMENT LEAN DIRECT INJECTOR
AN AUTOMATED ANALYTICAL DIFFERENTIA TION FRAMEWORK FOR REACTING FLOW SIMULATION
MESH-CONVERGED ADAPTIVE SIMULATIONS OF THE NASA ROTOR 37 TRANSONIC COMPRESSOR
COMPUTATIONAL AND EXPERIMENTAL ASSESSMENT OF RIM SEALING FLOWS IN AXIAL TURBINE CHUTE RIM SEALS
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
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
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
CHARACTERIZATION OF NON-REACTING SWIRLING FLOW IN A GAS TURBINE FUEL INJECTOR
SHOCK TUBE/LASER ABSORPTION MEASUREMENTS OF THE PYROLYSIS OF BUTYL ACETATE ISOMERS
EMISSIONS AND FLAME CHARACTERISTICS OF A HIGH-PRESSURE REACTING JET-IN-CROSSFLOW
NUMERICAL SIMULATION OF AN AXIAL REACTING JET-IN-CROSSFLOW AT ELEVATED PRESSURE