EFFECT OF VARIABLE INLET GUIDE VANES (VIGV) ON A SMALL GAS TURBINE ENGINE
DESIGN AND CHARACTERIZATION OF THE DUAL INDEPENDENT SWIRL COMBUSTOR FACILITY (DISCO)
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
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
NUMERICAL SIMULATION OF LEAN BLOWOUT OF ALTERNATIVE FUELS IN 7- ELEMENT 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