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

12 visualizaciones (últimos 30 días)
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...

Iniciar sesión para responder a esta pregunta.

Respuestas (0)

Categorías

Más información sobre Numerical Integration and Differential Equations en Help Center y File Exchange.

Etiquetas

Community Treasure Hunt

Find the treasures in MATLAB Central and discover how the community can help you!

Start Hunting!

Translated by