Sentence examples for inlet ratio from inspiring English sources

Also, the H2/COx inlet ratio may strongly influence the catalyst activity and selectivity.

In one example with an inlet ratio of 1 2 ethylene:isobutene at 500 °C and 1 bar, an outlet of 25% ethane and 21% isobutene was obtained.

The morphologies and composition of the as-grown CNNC arrays can be well controlled by regulating the methane/nitrogen mixture inlet ratio, and their optical absorption and resistivity strongly depend on their morphologies and composition.

In this work, a lumped mechanism is involved in a dynamic optimization procedure to reach a maximum efficiency of NO abatement in such devices, by handling the inlet ratio of H2 or CH4 to inlet NH3.

To achieve this goal, a set of steady-state Fischer Tropsch runs has been carried out in a lab-scale reactor loaded with a 20 wt.% Co/Al2O3 catalyst, investigating the effects of the main process conditions (temperature, H2/CO inlet ratio, content of inert gas in the feed, syngas space velocity) on the reactants conversion and on the C1 C50 product selectivity.

Analysis of product hydrogen gas deuterium enrichment was achieved using a dual inlet ratio mass spectrometer (VG Isogas 903D, Cheshire).

In the CNNC growth, the CH4/N2 inlet ratios were varied from 1/80 to 1/5 in order to obtain the CNNC arrays with different morphologies and compositions.

The temperature was varied from 420 to 500°C, the pressure from 1.6 to 16 bar, the molar H2/hydrocarbon inlet ratios from 1.5 to 20.

The effects of reaction temperature (550 700 °C), molar inlet ratios of carbon-to-oxygen (C/O = 0.75, 1.125; C and O: moles of carbon and oxygen atoms at the inlet, respectively) and steam-to-carbon (S/C = 3-5) and microchannel reactor configuration on product distribution and syngas composition were investigated.

The optimum inlet pressure ratio and fuel equivalence ratio at which the value of the specific thrust attains a maximum are presented.

An idealized thermodynamic cycle analysis is carried out to evaluate the performance of scramjet engines at different flight conditions, inlet pressure ratio and fuel equivalence ratio.