design of divergent part of nozzle with Rao's method for optimum thrust

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maziar
maziar el 10 de Jul. de 2021
Editada: maziar el 10 de Jul. de 2021
i need to use Rao's method for optimum thrust nozzle (based on method of characteristics) to design devergent part of nozzle and get the nozzle wall contour...

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