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
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
Kolbentriebwerk M 14 W 26 und Getriebe R-26 - Vorschrift für Betrieb
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
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
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
FLOW FIELD CHARACTERIZATION OF A THIRD GENERATION SWIRL-VENTURI LEAN DIRECT INJECTOR