학술논문

Aerodynamic design applying automatic differentiation and using robust variable fidelity optimization.
Document Type
Theses
Source
Dissertation Abstracts International; Dissertation Abstract International; 70-02B.
Subject
Engineering, Aerospace
Language
English
Abstract
Summary: Finally, the feasibility of reducing computational time for calculating derivatives and the necessity of AMF with an optimum design point always in the feasible region are discussed as future work.