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
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
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
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
AN AUTOMATED ANALYTICAL DIFFERENTIA TION FRAMEWORK FOR REACTING FLOW SIMULATION
MESH-CONVERGED ADAPTIVE SIMULATIONS OF THE NASA ROTOR 37 TRANSONIC COMPRESSOR
REQUIREMENTS TO ACHIEVE AFFORDABLE/SUSTAINABLE SPACE INFRASTRUCTURE
COMPUTATIONAL AND EXPERIMENTAL ASSESSMENT OF RIM SEALING FLOWS IN AXIAL TURBINE CHUTE RIM SEALS
DATA-DRIVEN COMBUSTION KINETIC MODELING CONCEPT OF ALTERNATIVE ALCOHOL-TO-JET (ATJ) FUEL
OPTIMAL SENSOR PLACEMENT FOR AZIMUTHAL ACOUSTIC MODE IN CYLINDRICAL DUCTS