Optimal Wing and Horizontal Tail Plane Design for Maximizing the Aircraft Performance in Cruise Flight-Reference-Cited by-同舟云学术

Optimal Wing and Horizontal Tail Plane Design for Maximizing the Aircraft Performance in Cruise Flight

Published:2022-01-25 Issue:3 Volume:54 Page:355-371
ISSN:0196-9722
Container-title:Cybernetics and Systems
language:en
Short-container-title:Cybernetics and Systems

Author:

Ferrero-Guillén Rubén¹^ORCID,Díez-González Javier¹^ORCID,Alija José Manuel¹^ORCID,Martínez-Gutiérrez Alberto¹^ORCID,Verde Paula¹^ORCID,Perez Hilde¹^ORCID

Affiliation:

1. Department of Mechanical, Computer and Aerospace Engineering, Universidad de León, León, Spain

Funder

Spanish Ministry of Science and Innovation

Publisher

Informa UK Limited

Subject

Artificial Intelligence,Information Systems,Software

Link

https://www.tandfonline.com/doi/pdf/10.1080/01969722.2022.2030010

Reference36 articles.

1. Aircraft design optimization

2. Studies in Aerodynamic Optimization Based on Genetic Algorithms

3. The historical fuel efficiency characteristics of regional aircraft from technological, operational, and cost perspectives

Cited by 6 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. On the selection of aircraft-engine pairs for medium-haul Low-Cost Carriers operations;Journal of Air Transport Management;2024-09

2. Black widow optimization for reducing the target uncertainties in localization wireless sensor networks;Logic Journal of the IGPL;2024-03-24

3. Parametric Study of NACA 4-Series Airfoil Designs for Lift-to-Drag Performance;J AERONAUT ASTRONAUT;2024

4. Aerodynamic Shape Optimization of Subsonic/Supersonic Flows Integrating Variable-Fidelity Longitudinal Trim Analysis;Aerospace;2024-02-08

5. Anti-vibration Design of the Civil Aircraft’s Horizontal Tail Trailing Edge Compartment;Journal of Physics: Conference Series;2023-11-01