Comprehensive Validation of Skeletal Mechanism for Turbulent Premixed Methane–Air Flame Simulations
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
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
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
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
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
EFFECT OF FUEL TEMPERATURE ON EMISSIONS AND STRUCTURE OF A SWIRLSTABILIZED FLAME
EFFECT OF FUEL TEMPERATURE ON EMISSIONS AND STRUCTURE OF A SWIRLSTABILIZED FLAME
LASER AND PARTICLE COUPLED BEAM PROPAGATION FOR DEEP SPACE PROPULSION
FOCUSING COMPRESSION DUE TO STEADY SUPERMULTI-JETS COLLIDING FOR AEROSPACE ENGINE
DYNAMICS OF THERMOACOUSTIC OSCILLATIONS IN A MULTI-NOZZLE COMBUSTOR
IMPACT ANALYSIS OF LIGHTWEIGHT DRONES ON BUSINESS JET ENGINE FAN BLADES