Optimal design for low sonic boom based on CoKriging surrogate model

• Published in: Hangkong Gongcheng Jinzhan Vol. 16; no. 3; pp. 60 - 69,81
• Main Authors: ZHANG Hanqi, XU Yue, ZHONG Min, LI Yan
• Format: Journal Article
• Language: Chinese
• Published: Editorial Department of Advances in Aeronautical Science and Engineering 01.06.2025
• Subjects: multi-fidelity; optimal design; sonic boom; supersonic civil aircraft; surrogate model

Accurately predicting and effectively reducing sonic boom levels is one of the key issues in the development of the new generation of green supersonic civil aircraft. In order to improve the efficiency of low sonic boom optimal design for supersonic civil aircraft, a multi-fidelity optimal design pr...