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...

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Autori principali:	Yu Wang, Qihang Li, Pan Li
Natura:	Artigo
Lingua:	Inglês
Pubblicazione:	MDPI AG 2025-11-01
Serie:	Aerospace
Soggetti:	tiltrotor vertical take-off and landing variable cycle engine vertical take-off & landing conceptual design aircraft sizing HSVTOL constraint analysis
Accesso online:	https://www.mdpi.com/2226-4310/12/11/992
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