Multifidelity Model–Assisted Knowledge Transfer Optimization Method for Computationally Intensive Solid Rocket Motor Design
Year: 2025
Type: article
Source: Journal of Aerospace Engineering
Authors: Jiawei Yang, Zeping Wu, Wenjie Wang, Weihua Zhang
Institution: National University of Defense Technology
Language: English
Subfield: Computational Theory and Mathematics
Field: Computer Science
Domain: Physical Sciences
Open Access status: closed
OpenAlex ID: W4412670643