EFFECT OF FUEL TEMPERATURE ON EMISSIONS AND STRUCTURE OF A SWIRLSTABILIZED FLAME
DYNAMICS OF THERMOACOUSTIC OSCILLATIONS IN A MULTI-NOZZLE COMBUSTOR
IMPACT ANALYSIS OF LIGHTWEIGHT DRONES ON BUSINESS JET ENGINE FAN BLADES
TURBULENT COMBUSTION MODELING OF A STAGED GAS TURBINE USING COMMERCIAL CFD CODE
LES/DNS OF FLOW PAST T106 LPT CASCADE USING A HIGHER-ORDER LB MODEL
Numerische Untersuchungen des Primärzerfalls an Kraftstoffdüsen für Flugtriebwerke
Einfluss pneumatischer Wirbelgeneratoren auf die Effektivität einer gekühlten Hochdruck-Turbine
NOX EMISSION OF AN AXIAL-STAGED COMBUSTOR AT HIGH-PRESSURE
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
DEVELOPMENT AND VALIDATION OF NON-AXISYMMETRIC BODY-FORCE PROPULSOR MODEL
AUTOIGNITION DELAY TIMES MEASUREMENTS OF LINEAR UNSATURATED JET FUEL COMPOUNDS INSIDE A SHOCK TUBE
EXPERIMENTAL AND NUMERICAL STUDIES OF SR30 TURBOJET ENGINE COMBUSTION
STEADY AND UNSTEADY FEATURES OF AN ELEVATED, PREMIXED, REACTING JET IN VITIATED CROSSFLOW
IGNITION OF CONVENTIONAL AND ALTERNATIVE JET FUELS AT ALTITUDE CONDITIONS
MODELING NON-PREMIXED JETS IN VITIATED CROSS FLOWS USING UNSTEADY FLAMELETS AND IN-SITU TABULATION
ANALYSIS OF GAS TURBINE COOLING TECHNOLOGIES FOR HIGHER NATURAL GAS COMBINED CYCLE EFFICIENCY
ANALYSIS OF TURBINE VISCOUS FLOW USING A NOVEL PROPER ORTHOGONAL DECOMPOSITION METHOD
LAMINAR BURNING VELOCITY MEASUREMENTS OF HIGH-PERFORMANCE JET FUEL/AIR MIXTURES
EFFECTS OF HIGH FREESTREAM TURBULENCE ON FILM COOLING EFFECTIVENESS OF SHAPED HOLES
FLOW FIELD ANALYSIS OF A DYNAMICALLY FORCED IMPINGEMENT JET ARRAY
ANALYSIS OF DISTORTION PHASE SHIFT IN A HIGHLY LOADED FAN STAGE
CHARACTERIZATION OF A LASER DIAGNOSTIC SENSOR FOR GAS TURBINE COMBUSTER FLOWS
DESIGN OPTIMIZATION OF DUMP DIFFUSERS WITH NACA 66-021 SHAPED FLAME TUBE
SPRAY VISUALIZATION AND CHARACTERIZATION OF A MULTI-JET CROSS-STREAM AIRBLAST INJECTOR
OPTIMIZATION ALGORITHM FOR AXIAL MULTISTAGE COMPRESSOR WORKFLOYW
DESIGN SPACE EXPLORATION OF FUTURE OPEN ROTOR CONFIGURATIONS
ROBUST, EFFICIENT AND ACCURATE MESH ADAPTATION FOR TURBOMACHINERY CFD SIMULATIONS
EXPERIMENTAL TEST RIG FOR 3D PRINTED, AXIAL COMPRESSOR UTILIZING A COTS TURBOCHARGER
AN INVESTIGATION INTO THE FEASIBILITY OF ALTERNATIVE AVIATION FUELS
DILUTED NATURAL GAS/OXIDIZER MIXTURES FOR ADVANCED ROCKET AND GAS
PREMIXED REACTING JET FLOW BEHAVIOR IN AN AXIALLY STAGED MODEL COMBUSTOR AT ELEVATED PRESSURE