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Aircraft design studies - vertical take off and landing airliner

open access: yes, 2022
During the 1970 academic year the students in Aircraft Design worked on the design of a vertical take off and landing airliner. The aircraft is intended to be capable of carrying up to 118 passengers over stage lengths of 500 n.miles.
Howe, D.
core   +3 more sources

DESIGN, BUILD AND FLY THE UITM’S VERTICAL TAKE-OFF AND LANDING (VTOL) AIRCRAFT

open access: yesMalaysian Journal of Computing, 2023
The aircraft with a vertical take-off and landing (VTOL) technology has been widely studied all around the world as it is one of the most advanced systems that could be used by modern aircraft.
Zurriati Mohd Ali   +2 more
doaj   +1 more source

Research on Transition Corridor of Ducted Vertical Take-off and Landing Fixed-wing UAV

open access: yesHangkong gongcheng jinzhan, 2022
The accurate description of the transition corridor is important for vertical take-off and landing(VTOL)fixed-wing unmanned aerial vehicle(UAV)flight. In order to study the transitional flight process of VTOL fixedwing UAV,a transition corridor model of ...
WANG Chunyang, ZHOU Zhou
doaj   +1 more source

Autonomous Transition Flight for a Vertical Take-Off and Landing aircraft [PDF]

open access: yesIEEE Conference on Decision and Control and European Control Conference, 2011
This paper addresses the problem of autonomous transition between hover and level flight for a model-scale fixed-wing Unmanned Air Vehicle (UAV). The UAV system is described as a Hybrid Automaton where the different operating modes correspond to the hover, transition, and level flight regions of the flight envelope. Reference maneuvers are generated so
Pedro Casau   +2 more
openaire   +2 more sources

The Performance of Airfoil with Lift Fan During Vertical Take-Off and Landing (VTOL) Condition [PDF]

open access: yes, 2016
This study investigated the performance of electric drive ducted lift-fan propeller in the airfoil during vertical take-off and landing (VTOL) condition.
Zulkefli, Nur Faraihan   +2 more
core   +2 more sources

Design and Fabrication of Small Vertical-Take-Off-Landing Unmanned Aerial Vehicle

open access: yesMATEC Web of Conferences, 2018
Modern UAVs available in the market have well-developed to cater to the countless field of application. UAVs have their own limitations in terms of flight range and manoeuvrability.
Abd Rahman Yasir Ashraf   +3 more
doaj   +1 more source

A Mobile Landing Platform for Miniature Vertical Take-Off and Landing Vehicles [PDF]

open access: yes2006 14th Mediterranean Conference on Control and Automation, 2006
Miniature Vertical Take-Off and Landing (VTOL) vehicles have limited range of operations mainly due to their limited payload capacities and power availability. To increase this range, a modified unmanned ground vehicle (UGV) is used to transport the VTOL to its target area serving as an on-site take-off/landing and possibly refueling base.
K. Dalamagkidis   +3 more
openaire   +2 more sources

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

open access: yesAerospace
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.
Yu Wang, Qihang Li, Pan Li
doaj   +1 more source

Study on Aerodynamic Characteristics of Tilting Wing Aircraft Considering Propeller Interference

open access: yesHangkong gongcheng jinzhan, 2019
Tilting wing aircraft not only has the ability of vertical take-off and landing like helicopter, but also be provided with high speed cruise capability as traditional fixed-wing aircraft.Tilting wing aircraft is one of the hot spots of research in both ...
Wei Wei   +3 more
doaj   +1 more source

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