Strong selection pressure on the immune system to cope with changing environment and disease, and response to stress, drive the selection on these genes over a broad evolutionary time-spectrum.
Finally, the impact of pressure and equivalence ratio on ignition delay time is evaluated over a broad range of pressure (1 50 bar) and equivalence ratio (ϕ = 0.2 3).
Reasonable agreements between calculated and measured values of propellant burning rates and surface temperatures were obtained over a broad range of pressure from 0.7 to 350 atm.
A comprehensive numerical analysis has been developed to predict the burning characteristics and detailed combustion wave structure of RDX/GAP/BTTN pseudo-propellant over a broad range of pressures.
This flexibility in the choice of sample pressure provides a route for downstream integration with a large set of classical and emerging ionization methods operating over a broad range of pressures, including ambient and subambient, coupled to active and passive sampling methods.
Complex chemistry calculations carried out over a broad range of operating pressures indicate that the pressure dependences deduced analytically are remarkably accurate and can be used for a broad range of strain rates, excluding values in the near vicinity of extinction conditions, where finite rate chemistry effects become important and influence the flame response to pressure.
The simulations are in qualitative and quantitative agreement with measurements over a broad ranges of temperature, pressure, and composition.
The usual validation procedure of a kinetic scheme consists in graphically comparing numerical simulations with the widest set of experimental data, with the goal of proving the model predictive capabilities over a broad range of temperature, pressure, and dilution conditions.
A comprehensive numerical analysis of HMX/GAP pseudo-propellant combustion has been established to predict the propellant burning rate and detailed combustion wave structure over a broad range of ambient pressure, laser intensity, and propellant composition.
