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The water storage rate, water flooding index and the recovery degree are the important indexes which reflect the development effect of the water injection field.
Our results show that the injection orifice surely has a great scale effect on the transversal injection field in cold kerosene-fueled supersonic flows.
The incident shock wave generally has a strong effect on the transversal injection field in cold kerosene-fueled supersonic flow, possibly due to its affecting the interaction between incoming flow and fuel through various operation conditions.
The capture of such electrons can cause a change of trapped charge (ΔQ = ne) as well as a shift of local injection field (ΔEL) [45, 46]: Δ Q = C ⋅ Δ V = ϵ GeO 2. Φ t GeO 2 Δ V, (2) Δ E L = Δ V t GeO 2 = ne ϵ GeO 2. Φ, (3).
Patient blinding was ensured by avoiding visual access to the injection field (eg, by a screen between the patient and his/her knee).
On the other hand, double-blind conditions were ensured by nominating at each site an 'injector' and a blinded 'assessor' investigator, while avoiding the patient's visual access to the injection field.
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These trapped charges change the injection fields and, thus, the amount of charge transferred to and from the charge storage layer during programming.
In the current study, the transverse injection flow field with a freestream Mach number of 3.5 has been optimized by the non-dominated sorting genetic algorithm (NSGA II) coupled with the Kriging surrogate model; and the variance analysis method and the extreme difference analysis method have been employed to evaluate the values of the objective functions.
The obtained results show that the jet-to-crossflow pressure ratio is the most important design variable for the transverse injection flow field, and the injectant molecular weight and the slot width should be considered for the mixing process between the injectant and the supersonic crossflow.
In the current study, the three-dimensional Reynolds-averaged Navier Stokes (RANS) equations coupled with the two equation SST k-ω turbulence model has been utilized to simulation the transverse injection flow field with a freestream Mach number 3.75, and the influence of the turbulence model on the flow field properties has been evaluated as well.
The injector length is chosen as design variable for analysis of reverse fuel injection flow field.
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