Results 31 to 40 of about 1,986 (195)
Three-Dimensional Flight Envelope for V/STOL Aircraft with Multiple Flight Modes
Vertical or short take-off and landing (V/STOL) aircraft generally have three flight modes, namely, vertical take-off and landing (VTOL), conversion, and cruise, according to the variable angle of propulsion direction to the fuselage axis.
Tielin Ma +4 more
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Whirl Flutter Suppression of Tiltrotor Aircraft Using Actively Controlled Aileron
Whirl flutter of a tiltrotor aircraft is a complex aeroelastic phenomenon and it can result in catastrophic consequences. The deflection of an aileron mounted on a wing has the potential to solve this fatal problem.
Linghua Dong, Qiyu Li
doaj +1 more source
Quad-Tiltrotor – modelling and control [PDF]
Aircrafts with VTOL capabilities announced a new era in marine aviation. Their aerodrome requirements, which are as low as for helicopters, make them excellent candidates for many missions required...
Marcin Ciopcia, Cezary Szczepański
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The tiltrotor wing structure is one of the most critical and heavily investigated structures in design due to the fundamental need to consider the interactions between the wing, pylon, and rotor systems to achieve aircraft aeroelastic stability.
Aniello Daniele Marano +8 more
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Integration of Sensors in Control and Automation Systems 2020
Journal of Sensors, Volume 2022, Issue 1, 2022.
Rafael Morales +3 more
wiley +1 more source
Development and design of tiltrotor nacelle's (NGCTR)
TRAIL - Design, manufacture and deliver a high performance, low cost, low weight Nacelle Structure for Next Generation Tilt-Rotor (NGCTR), Clean Sky 2 Joint Undertaking, European Union (EU), Horizon 2020 EU Grant agreement ID: 864726 DISCLAIMER “The content of this document reflects only the author’s view.
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Numerical simulations on the ERICA tiltrotor [PDF]
This paper presents aerodynamic calculations of the model-scale ERICA tiltrotor with high-fidelity\ud computational fluid dynamics. The aim of this work is to assess the capability of the present CFD\ud method in predicting airloads on the tiltrotor at different flight configurations. In this regard, three\ud representative flight configurations of the
Jimenez Garcia, Antonio +1 more
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Assessment of a Mid-Fidelity Numerical Approach for the Investigation of Tiltrotor Aerodynamics
The study of the complex aerodynamics that characterise tiltrotors represents a challenge for computational fluid dynamics tools. URANS numerical solvers are typically used to explore the aerodynamic features that characterise the different flight ...
Alex Zanotti +4 more
doaj +1 more source
Design and Implementation of a Hardware‐in‐the‐Loop Simulation System for a Tilt Trirotor UAV
The tilt trirotor unmanned aerial vehicle (UAV) is a novel aircraft that has broad application prospects in transportation. However, the development progress of the aircraft is slow due to the complicated control system and the high cost of the flight experiment.
Li Yu +5 more
wiley +1 more source
Minimally Actuated Tiltrotor for Perching and Normal Force Exertion
This study presents a new hardware design and control of a minimally actuated 5 control degrees of freedom (CDoF) quadrotor-based tiltrotor. The proposed tiltrotor possesses several characteristics distinct from those found in existing works, including: 1) minimal number of actuators for 5 CDoF, 2) large margin to generate interaction force during ...
Dongjae Lee +4 more
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