The goal of this study was to collect and organize the information for inclusion in an intermediate course in turbomachines. It has been subsequently modified and extended in many studies and is still under active develop- ment. The derivatives at the endpoints of each data set are calculated differently than any non endpoint. Since the flow is inviscid and irrotational, the Bernoulli equation can be used between any points in the flow. Since much work has gone into the development of the streamline curvature meth- ods over the last half century, it is difficult to make any new contributions to the subject.
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