Abstract: Empirical formulae are presented by means of which the partial pressures of CO2 and H2 O in the combustion gases of aviation fuel-air and diesel fuel-air systems can be calculated as functions ...

Abstract: An approximate formula is presented by means of which the adiabatic flame temperature of jet fuel-air systems can be calculated as functions of pressure, temperature, equivalence ratio, and ...

Abstract: The smoke point has been shown to be quantitatively related to the molecular structure of hydrocarbon fuels. A fast technique of determining the molecular composition of commercial and experimental ...

Abstract: A systematic study of soot formation along the centerlines of axisymmetric laminar diffusion flames of a large number of liquid hydrocarbons, hydrocarbon blends, and aviation turbine and diesel ...