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Turbomachinery Aerodyanmics

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Turbomachinery Aerodyanmics ( turbomachinery-aerodyanmics )

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was much later; that it was also being considered as one of the options for use in gas turbine engine. And, the modern day gas turbine technology has restricted the use of radial flow turbines. It is primarily used in the smaller engines, smaller thrust class engines. And, it is the main disadvantage, when it comes to use of radial flow turbines; for gas turbine applications, is the fact that in order to achieve very high efficiencies and power output, the turbine performance is a strong function of the inlet temperature. And in axial turbines, we have already discussed that modern day gas turbines use different cooling technologies, which can be used to, which can actually permit us to use turbine...temperatures, which are much higher than their material limits. This is not. It is still possible in radial flow turbines, but it is it is much more complicated to introduce and use some sort of cooling mechanisms in radial flow turbines. There are complicated methods, which are being proposed and probably being used in some types of engines. And, this is one major disadvantage. While radial turbines are not really used in gas turbine technology, in gas turbine engines, for larger thrust class engines because the turbine inlet temperature is sort of restricted. We saw that there are two different types of inward flow turbines: the cantilever type and the 90 degree inward flow turbines. And, we discussed in the previous class. We devoted most of the time towards discussion on the 90 degree inward flow turbine because that is more commonly used. The cantilever type turbine is very similar to the impulse turbine that we have already discussed in the axial turbine context. And therefore, there are certain disadvantages associated with impulse turbine as we have already seen. And, so the inward flow, 90 degree inward flow turbine is like reaction turbine. And, in geometrical terms, a 90 degree inward flow turbine looks exactly similar to a centrifugal compressor. And, but of course, just at the direction of flow and the rotation of the impeller or the rotor is exactly opposite in each cases. We also discussed about the governing equations, which are used when we analyze the flow in these different components. Starting from the outlet flow, the volute or the scroll, and then the nozzle blades, and then it goes into the rotor or impeller. And then, there is the exducer, which forms the later part of the impeller. Its counterpart and centrifugal

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