Results 11 to 20 of about 19,013 (214)

Study on the Selection Method of Power Unit for Manned Multi-rotor Aircraft

open access: yesHangkong gongcheng jinzhan, 2021
The manned multi-rotor aircraft has the characteristics of large structural size, large load demand, and variable size and variable number of available rotors.The rapid determination of the power unit of this type of aircraft is of strong engineering ...
CHEN Sijing   +4 more
doaj   +1 more source

Generalized Quantitative Stability Analysis of Time-Dependent Comprehensive Rotorcraft Systems

open access: yesAerospace, 2021
Rotorcraft stability is an inherently multidisciplinary area, including aerodynamics of rotor and fuselage, structural dynamics of flexible structures, actuator dynamics, control, and stability augmentation systems.
Aykut Tamer, Pierangelo Masarati
doaj   +1 more source

Fuzzy Neural Network PID Control Used in Individual Blade Control

open access: yesAerospace, 2023
In order to further reduce the vibration level of helicopters, the active vibration control technology of helicopters has been extensively studied. Among them, individual blade control (IBC) independently applies high-order harmonics to each blade with ...
Renguo Yang   +3 more
doaj   +1 more source

Analysis of the Aeroacoustic Characteristics of a Rigid Coaxial Rotor in Forward Flight Based on the CFD/VVPM Hybrid Method

open access: yesAerospace, 2023
This study develops a hybrid solver with reversed overset assembly technology (ROAT), a viscous vortex particle method (VVPM), and a CFD program based on the URNS method, in order to study the aerodynamic and acoustic characteristics of coaxial rigid ...
Yucheng Yang   +3 more
doaj   +1 more source

Numerical Simulation of Tiltrotor Flow Field during Shipboard Take-Off and Landing Based on CFD-CSD Coupling

open access: yesAerospace, 2022
Due to the small tilt angle, a tiltrotor operates in non-axial flow conditions during shipboard take-off and landing. The non-uniformity of the blade’s air-load is high, resulting in structural deformation with high fluctuation frequency, affecting the ...
Peng Yu   +3 more
doaj   +1 more source

Particularities of Rotorcraft in Dealing with Advanced Controllers [PDF]

open access: yesINCAS Bulletin
Advanced nonlinear controllers are a desirable solution to rotorcraft flight control as they can solve the system high nonlinear dynamic behavior. However, conventional nonlinear controllers such as Nonlinear Dynamic Inversion (NDI) controller heavily ...
Marilena D. PAVEL
doaj   +1 more source

Geometry Design of Coaxial Rigid Rotor in High-Speed Forward Flight

open access: yesInternational Journal of Aerospace Engineering, 2020
The aerodynamic performance analysis and blade planform design of a coaxial rigid rotor in forward flight were carried out utilizing CFD solver CLORNS. Firstly, the forward flow field characteristics of the coaxial rotor were analyzed.
Bo Wang   +3 more
doaj   +1 more source

Conversion Flight Control for Tiltrotor Aircraft via Active Disturbance Rejection Control

open access: yesAerospace, 2022
The tiltrotor aircraft consists of three primary flight modes, which are helicopter flight mode in low forward speed flight, airplane flight mode in high forward speed flight and conversion flight mode. This paper presents an active disturbance rejection
Ke Lu   +4 more
doaj   +1 more source

Numerical Research on the Layout for Wing-Deflectable Hydrofoil Seaplane

open access: yesHangkong gongcheng jinzhan, 2019
Aiming at the problem of big drag during takeoff for seaplane, a hydrofoil seaplane with deflectable wings is proposed. The hydrodynamic lift generated by deflectable wing cutting the water surface during takeoff is big enough to lift the aircraft off ...
Shen Suiyuan   +4 more
doaj   +1 more source

Analysis of Rotor/Propeller/Fuselage Interaction Characteristics of High-speed Helicopter

open access: yesHangkong gongcheng jinzhan, 2020
The study on aerodynamic characteristics of high-speed helicopter with double-thrust-propeller can provide the reference for the design and aerodynamic optimization of high-speed helicopter.
SHEN Suiyuan   +4 more
doaj   +1 more source

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