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GC analyses were carried out using a Perkin Elmer Autosystem GC apparatus (Walhton, MA, USA) equipped with a single injector and two flame ionization detectors (FID).
To determine the effect fracture surface variations have on fluid flow and on a reservoir's thermal performance, a dipole flow in circular fractures between a single injector and producer was selected.
First, acoustic behavior in the combustor with a single injector is investigated and acoustic-damping effect of the injector is evaluated for cold condition by the quantitative parameter of damping factor as a function of injector length.
The measured change in the behavior of single bubbles injected into the pulp slurry through a single injector, is the basis for a proposed mechanism for the increased bubble coalescence in a multi-bubble system.
Analytical GC was carried out in a Hewlett-Packard 6890 (Agilent Technologies, Palo Alto, CA, USA) chromatograph with a HP GC ChemStation Rev. A.05.04 data handling system, equipped with a single injector and two flame ionization detectors (FIDs).
Intramammary administration was made through teat with a single injector containing an enrofloxacin suspension (1 g of enrofloxacin/5 g of ointment) via the teat canal, massaging afterwards into the gland cistern.
Similar(54)
The model has been validated and successfully applied to the computation of 0D phase change with heat addition, and a supercritical reactive coaxial LOX/GH2 single injector.
PLIF is used to examine jet flames formed by a single coaxial injector fed by liquid oxygen and gaseous hydrogen (LOx/GH2) in subcritical and transcritical regimes.
The bubble characteristics of bubbles injected through a single bubble injector are studied in a small rectangular column through the use of flow visualization and a particle image velocimetry technique.
In the first study, the effect of inlet pressure is investigated by using a series of different rail pressures in both numerical and experimental tests in a single hole industrial injector.
This paper describes a numerical study of a strong ignition sequence observed in a laboratory-scale single-injector rocket chamber ignited by a laser and fueled with gaseous oxygen and hydrogen.
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