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

12 visualizzazioni (ultimi 30 giorni)
maziar
maziar il 10 Lug 2021
Modificato: maziar il 10 Lug 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...

Accedi per rispondere a questa domanda.

Risposte (0)

Categorie

Scopri di più su Numerical Integration and Differential Equations in Help Center e File Exchange

Tag

Community Treasure Hunt

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

Start Hunting!

Translated by