design of divergent part of nozzle with Rao's method for optimum thrust
6 vues (au cours des 30 derniers jours)
Afficher commentaires plus anciens
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...
0 commentaires
Réponses (0)
Voir également
Catégories
En savoir plus sur Wind Power dans Help Center et File Exchange
Community Treasure Hunt
Find the treasures in MATLAB Central and discover how the community can help you!
Start Hunting!