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Key aspects of electric vertical take-off and landing conceptual design
- Publication Year :
- 2019
- Publisher :
- SAGE, 2019.
-
Abstract
- The recent advances in battery energy density and electric propulsion systems for automotive applications are enabling the development of the electric vertical take-off and landing (VTOL) aircraft. The electric VTOL is a new means of transport that can fly like an aircraft and take off and land vertically like a helicopter, sometimes called personal aerial vehicle. This paper compares it to the existing vehicles that may compete with it and addresses the estimation of its performances in hover, cruise flight, and the transition phase. The main parameters affecting performances are then discussed. Considerable space is dedicated to the battery mass to total mass ratio.
- Subjects :
- Battery energy
Electric vertical take-off and landing aircraft, range, hover, transition, personal aerial vehicle
Engineering
business.industry
Mechanical Engineering
Automotive industry
personal aerial vehicle
Aerospace Engineering
hover
transition
Electric vertical take-off and landing aircraft
Conceptual design
Electrically powered spacecraft propulsion
Range (aeronautics)
range
Key (cryptography)
Aerospace engineering
business
Vertical take off and landing
Subjects
Details
- Database :
- OpenAIRE
- Accession number :
- edsair.doi.dedup.....1965fb012dad4c2d487f93bd0ef33526