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Velocity profiles at the inlet and exit sections are measured with hot-wire anemometer.
The turbine is designed for inlet and exit temperatures of 24.5 °C and 14 °C respectively.
The inlet and exit coolant temperatures are 340 and 490 °C, respectively, in the core.
The absolute inlet and exit angles of the rotor are taken as design variables.
The absolute inlet and exit angles of the rotor, the absolute exit angle of the stator, and the relative gas densities at the inlet and exit stations of the stator, of every stage, are taken as the design variables.
The longer inlet and exit ducts provide scope to further reduce engine noise by allowing additional acoustic liners, compared to conventional nacelles, to absorb the engine noise.
Similar(10)
Fig. 2 Schematic of ALD chamber: a the precursors and N2 gas are pulsed in through the gas inlets and exit through the exhaust, making the gas flow from left to right over the silver knife.
The EES model developed for ejector nozzles can be used to design any supersonic nozzle for the desired inlet and outlet pressers and exit velocity.
Through the CFD simulations, the similarity of the temperature rise was demonstrated well between the inlet and the exit, and the exit temperature was well maintained between the prototype and the half scale model.
Inlet and outlet gas lines exit through the chest wall.
The chimney inlet area and exit areas are equal.
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