Modern military aircraft use jet fuel as a coolant before it is burned in the combustor. Prior to combustion, dissolved O-2 and trace heteroatomic species react with the heated fuel to form insoluble parades and surface deposits that an impair engine performance. For safe aircraft,operation, it is important to minimize jet fuel oxidation and resultant surface deposition in critical fuel system components. ASTM D3241, "Standard Test Method for Thermal Oxidation Stability of Aviation Turbine Fuel" (ASTM International: West Conshohocken, PA, 2014), defines the standard test method for evaluation of the thermal oxidation stability of aviation turbine fuels. The JFTOT is a thermal stability test that measures the tendency for fuel to form deposits via heated tube discoloration and/or an increased pressure drop across an outlet filter. It is used to discriminate between fuels of poor and acceptable thermal stability. However, the fluid dynamics, transfer characteristics, extent Of oxidation, and corresponding deposition that occurs in the JFTOT are not fully understood. An improved understanding of these JFTOT characteristics should help in the interpretation of conventional and alternative fuel thermal stability measurements and provide important information for fuel thermal stability specification enhancements and revisions. In the current effort, the JFTOT was modified to include a bulk Outlet thermocouple measurement and a downstream oxygen sensor to measure bulk oxygen consumption. Tube deposition profiles were measured via ellipsometry. External tube wall temperatures were-measured via pyrometry and a,computational fluid dynamic (CFD) with chemistry simulation was developed. The experimental temperature Measurements show that the cooling of the outlet bus bar creates a wall hot tone near the center of the tube length. A direct relationship is found between the bulk outlet temperature and JFTOT set point temperature with the bulk outlet less than-the Set point temperature by 60-85 degrees C. Several fuels were tested at varying set point temperatures with complete oxygen consumption observed for all fuels by 320 degrees C; a wide oxygen consumption range from 10% to 85% was measured at a set point temperature of 260 degrees C. The CFD simulations demonstrated the importance of complex, three dimensional flows on the hear transfer, oxygen consumption and deposition: These three-dimensional simulations showed considerable flow recirculation due to buoyancy effects, which resulted in complex fuel residence time behavior. An optimized chemical kinetic model of autoxidation with a global deposition submechanism is able to reprodute the observed oxidation-and depositions characteristic of the JFTOT. Simulations of deposition were of the right order of magnitude and matched the deposit profile of comparable experimental ellipsometric deposition data. This improved CFD with chemistry-simulation provides the ability to predict the, location and quantity of oxygen consumption and deposition over a Wide range of temperatures and conditions relevant to jet fuel system operation.