Low fidelity data driven machine learning based optimisation method for box-wing configuration-Reference-Cited by-同舟云学术

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Low fidelity data driven machine learning based optimisation method for box-wing configuration

Published:2024-07 Issue: Volume:150 Page:109169
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Hasan Mehedi^ORCID,Khandoker Azad^ORCID,Gessl Guido^ORCID,Hamid M.A.,Ali Mohammed

Publisher

Elsevier BV

Reference62 articles.

1. Data-based approach for wing shape design optimization;Li;Aerosp. Sci. Technol.,2021

2. Aerodynamic optimization of box wing - A case study;Khalid;Int. J. Aviation Aeronaut. Aerospace,2014

3. L. Prandtl, “Induced drag of multiplanes,” Washington, DC, 1924. [Online]. Available: https://ntrs.nasa.gov/api/citations/19930080964/downloads/19930080964.pdf.

4. The PrandtlPlane configuration: overview on possible applications to civil aviation;Frediani,2012

5. Understanding box wing aircraft: essential technology to improve sustainability in the aviation industry;Somerville;Aviation,2016

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Enhancing box-wing design efficiency through machine learning based optimization;Chinese Journal of Aeronautics;2024-09

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