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The combustion gas temperature varied between 1500 and 1800 K.
Resilient chromium-niobium material for industrial processes including coal and petroleum combustion, gas turbines, and waste incinerators.
Among the required combustion gas properties provided by solid propellant gas generators, the combustion gas temperature should not exceed a certain temperature which may damage the turbine blades.
This combustion gas was cooled further (by steam injected into it) to 400° C, the maximum temperature that Elling's radial-inflow turbine could handle.
Due to the low concentration of CO2 in the post combustion gas, this requires large scale equipment, able to process large quantities of gas.
The RNG k ε model is employed in the numerical simulation of turbulent combustion gas flow.
Single-cylinder and two-cylinder engines were analyzed using a preheater and CGR (combustion gas recirculation).
The rocket nozzle throat is exposed to combustion gas of high temperature.
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The sensor detects oxygen and/or incomplete-combustion gas concentration in exhaust to find the A/F of engine operations.
This paper explores dynamics for control design of a Hydrogen Membrane Reformer (HMR) pre-combustion gas power cycle.
Carbon monoxide and nitric oxide exist in post-combustion gas streams and can therefore influence CO2 transport through membranes designed for that application.
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