Open AccessThe Method for Optimum Design of Water Rocket Flight Stability Performance Conditions Using CAE with T Method and Robust Parameter Design
Author(s) -
Eiji Toma,
Yoshihiro Ito
Publication year - 2021
Publication title -
journal of applied mathematics and physics
Language(s) - English
Resource type - Journals
eISSN - 2327-4379
pISSN - 2327-4352
DOI - 10.4236/jamp.2021.911172
Subject(s) - rocket (weapon) , aerospace engineering , thrust , stability (learning theory) , computer science , flight dynamics , aerodynamics , simulation , engineering , machine learning