Multi-Point Aerodynamic Optimization Design of Wide-Speed-Range Airfoils

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

In this work, an optimization framework based on surrogate model is constructed for airfoil aerodynamic optimization in a wide-speed-range environment. The geometrical change law of airfoils under different design parameters is investigated. The results indicate that, when considering both subsonic and super-sonic aerodynamic characteristics of the airfoil, as the weight of supersonic aerodynamics.

Original languageEnglish
Title of host publicationMechanical and Aerospace Engineering - Proceedings of the 15th International Conference, ICMAE 2024
EditorsPasquale Daponte
PublisherIOS Press BV
Pages539-549
Number of pages11
ISBN (Electronic)9781643685984
DOIs
StatePublished - 16 Jun 2025
Event15th International Conference on Mechanical and Aerospace Engineering, ICMAE 2024 - Zagreb, Croatia
Duration: 17 Jul 202420 Jul 2024

Publication series

NameAdvances in Transdisciplinary Engineering
Volume71
ISSN (Print)2352-751X
ISSN (Electronic)2352-7528

Conference

Conference15th International Conference on Mechanical and Aerospace Engineering, ICMAE 2024
Country/TerritoryCroatia
CityZagreb
Period17/07/2420/07/24

Keywords

  • Wide-speed-range configuration
  • airfoil optimization
  • gradient optimization design
  • surrogate model

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