Effect of angle of attack variation on turboprop engine performance: a digital twin-based approach

Ayşe Nur Dişlitaş; Elif Zeyneb Tekin; Melih Yıldız; Artūras Kilikevičius; Utku Kale

doi:10.1007/s10973-026-16301-w

Publications › Aircraft design, systems thinking and digital twins

Aircraft design, systems thinking and digital twinsArticle

Effect of angle of attack variation on turboprop engine performance: a digital twin-based approach

Ayşe Nur Dişlitaş, Elif Zeyneb Tekin, Melih Yıldız, Artūras Kilikevičius, Utku Kale

Journal of Thermal Analysis and Calorimetry, 2026 · Springer Science and Business Media LLC

Abstract

Abstract to be added from the published version.

Read at publisher (DOI)Google Scholar

A General Electric CF6 turbofan engine mounted in a test cell.Photo: · public domain · Wikimedia Commons

Keywords

angle of attacksurge margindigital twinspecific fuel consumptionregional aircraftwing stallAMESim

DOI

10.1007/s10973-026-16301-w

Cite · BibTeX

@article{dilita2026effect,
  title = {Effect of angle of attack variation on turboprop engine performance: a digital twin-based approach},
  author = {Ayşe Nur Dişlitaş and Elif Zeyneb Tekin and Melih Yıldız and Artūras Kilikevičius and Utku Kale},
  journal = {Journal of Thermal Analysis and Calorimetry},
  year = {2026},
  publisher = {Springer Science and Business Media LLC},
  doi = {10.1007/s10973-026-16301-w},
}