Aerostructural Design Optimization Using a Multifidelity Quasi-Newton Method
Sign Up to like & getrecommendations! Published in 2019 at "Journal of Aircraft"
DOI: 10.2514/1.c035152
Abstract: The traditional aircraft design process relies upon low-fidelity models for expedience and resource savings. However, the reduced accuracy and reliability of low-fidelity tools often lead to the di... read more here.
Keywords: aerostructural design; optimization using; design; using multifidelity ... See more keywords