Optimal design for low sonic boom based on CoKriging 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...
Saved in:
Main Authors: | ZHANG Hanqi, XU Yue, ZHONG Min, LI Yan |
---|---|
Format: | Article |
Language: | Chinese |
Published: |
Editorial Department of Advances in Aeronautical Science and Engineering
2025-06-01
|
Series: | Hangkong gongcheng jinzhan |
Subjects: | |
Online Access: | http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2023278 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
A Numerical Approach for the Integration of Sonic Boom Requirements into the Matching Chart
by: Samuele Graziani, et al.
Published: (2025-06-01) -
Sonic Boom Impact Assessment of European SST Concept for Milan to New York Supersonic Flight
by: Giovanni Fasulo, et al.
Published: (2025-05-01) -
SCGAN-enhanced surrogate modeling for FEM analysis of induction motors: A practical use case
by: Unai Salaberria-Flaño, et al.
Published: (2025-09-01) -
Aerodynamic optimization of a coaxial rotor system using a deep learning-based multi-fidelity surrogate model
by: Shu-Hui Qin, et al.
Published: (2025-12-01) -
The Reliability Analysis of a Turbine Rotor Structure Based on the Kriging Surrogate Model
by: Haiwei Lin, et al.
Published: (2025-07-01)