Estimation Method for Basic Parameters of High-Speed Vertical Take-Off and Landing Aircraft

The research aims to propose a basic parameter estimation method for high-speed vertical take-off and landing (HSVTOL) aircraft, balancing rotor and fixed-wing mode requirements. Flight profiles and performance indicators are defined based on mission phases, and maximum take-off weight is estimated...

Ausführliche Beschreibung

Bibliografische Detailangaben

Hauptverfasser:	Yu Wang, Qihang Li, Pan Li
Format:	Artigo
Sprache:	Inglês
Veröffentlicht:	MDPI AG 2025-11-01
Schriftenreihe:	Aerospace
Schlagworte:	tiltrotor vertical take-off and landing variable cycle engine vertical take-off & landing conceptual design aircraft sizing HSVTOL constraint analysis
Online-Zugang:	https://www.mdpi.com/2226-4310/12/11/992
Tags:	Tag hinzufügen Keine Tags, Fügen Sie das erste Tag hinzu!