Results 31 to 40 of about 22,232 (271)

A Single Oscillator-Excited Piezoelectric Actuator with Internal Contact Teeth

open access: yesMicromachines, 2023
The tail rotor of a helicopter, a crucial component, traditionally relies on a complex drive mode involving reducers and transmission gears. This conventional setup, with its lengthy transmission chain and numerous components, hinders miniaturization ...
Die Fang   +7 more
doaj   +1 more source

Numerical analysis for main-rotor/tail-rotor interaction of helicopter

open access: yesNumerical analysis for main-rotor/tail-rotor interaction of helicopter, 2008
A simulation method for full helicopter configuration is constructed by combining an unsteady Euler code and an aeroacoustic code based on the Ffowcs-Williams and Hawkings formulation. The flow field and helicopter noise are calculated using a moving overlapped grid system, and the mutual effect of main rotor and tail rotor are studied for the ...
YANG, Choongmo   +3 more
openaire   +2 more sources

The flow field around a rotor in axial descent [PDF]

open access: yes, 2005
Measurements of the flow field around a model rotor descending axially into its own vortex wake have been performed using particle image velocimetry (PIV). At low descent rates, the expected cylindrical down-flow structure below the rotor is observed. At
Brown, R.E., Gillies, E.A., Green, R.B.
core   +1 more source

THE EFFECT OF DIFFERENT OPTIONS OF BLADES MAIN ROTOR ON THE X-SHAPED TAIL ROTOR OF THE MI-171 LL

open access: yesНаучный вестник МГТУ ГА, 2018
This paper describes the effect of different rotor blades on the X-shaped tail rotor of the Mi-171 LL, observed conducting flight tests. The tests were carried out on the same helicopter in the similar atmospheric conditions.The objective of the tests ...
V. A. Ivchin   +2 more
doaj   +1 more source

Robust Flat Filtering Control of a Two Degrees of Freedom Helicopter Subject to Tail Rotor Disturbances

open access: yesInternational Journal of Applied Mathematics and Computer Science, 2023
This article deals with modelling and a flatness-based robust trajectory tracking scheme for a two degrees of freedom helicopter, which is subject to four types of tail rotor disturbances to validate the control scheme robustness. A mathematical model of
Sánchez-Meza Victor-Gabriel   +4 more
doaj   +1 more source

Imaging and Motion Parameter Estimation of Flying Helicopter With Duo Airborne SARs in $X$-Band

open access: yesIEEE Journal of Selected Topics in Applied Earth Observations and Remote Sensing, 2022
Duo airborne synthetic aperture radars in the $X$-band are proposed to acquire images of a flying helicopter. The backscattered signals manifest entangled features attributed to the compound linear motion of fuselage and spin motion of rotors.
Chou-Wei Kiang, Jean-Fu Kiang
doaj   +1 more source

Experimental research of single - rotor helicopter unintentional yaw rotation

open access: yesНаучный вестник МГТУ ГА, 2020
Aviation accidents related to unintentional rotation may periodically occur while flying single-rotor helicopters. On-time and correct actions may help the pilot to find the way out of this hazardous situation.
V. V. Efimov   +3 more
doaj   +1 more source

Design and Determination of Aerodynamic Coefficients of a Tail-Sitter Aircraft by Means of CFD Numerical Simulation

open access: yesMachines, 2022
Vertical take-off and landing (VTOL) aircraft have become important aerial vehicles for various sectors, such as security, health, and commercial sectors.
Emmanuel Alejandro Islas-Narvaez   +4 more
doaj   +1 more source

Simulation of wind turbine wake interaction using the vorticity transport model [PDF]

open access: yes, 2010
The aerodynamic interactions that can occur within a wind farm can result in the constituent turbines generating a lower power output than would be possible if each of the turbines were operated in isolation.
Fletcher, Timothy M.   +5 more
core   +1 more source

Modelling the aerodynamics of coaxial helicopters : from an isolated rotor to a complete aircraft [PDF]

open access: yes, 2008
This paper provides an overview of recent research on the aerodynamics of coaxial rotors at the Rotorcraft Aeromechanics Laboratory of the Glasgow University Rotorcraft Laboratories.
Brown, R.E.   +5 more
core   +1 more source

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