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