Results 31 to 40 of about 7,767,476 (330)

Application of pressure head theory to determine the aerodynamic characteristics of the helicopter main rotor [PDF]

open access: yesE3S Web of Conferences, 2021
A method is proposed for calculating main aerodynamic characteristics of the main rotor of the Mi-26 helicopter: a lift, a reactive moment, a required power of the propulsion system, a speed of the inductive air flow, a throttle response coefficient, a ...
Reshenkin Andrey   +3 more
doaj   +1 more source

Rotor Flux Controller for Induction Machines Considering Main Inductance Saturation [PDF]

open access: yesProblems of the Regional Energetics, 2020
This paper discusses the problem of controlling electromechanical systems with maximum per-formance while maintaining accuracy and minimum power consumption.
Diachenko G.
doaj   +1 more source

Mathematical description of the interaction between a probing microwave signal and the helicopter main rotor blade

open access: yesВестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, 2016
The paper deals with the non-contact method of monitoring the integrity of the main rotor blades of a helicopter. The available methods of monitoring the integrity of the main rotor blades of the helicopter are labor-intensive to implement, their ...
A. I. Danilin, S. V. Zhukov, M. S. Popov
doaj   +1 more source

Aerodynamic Characteristics of Helicopter with Ducted Fan Tail Rotor in Hover under Low-Speed Crosswind

open access: yesInternational Journal of Aerospace Engineering, 2020
The tail rotor of a helicopter operating under low-speed crosswind undergoes highly complex flow due to the interaction between the main rotor, fuselage, and tail rotor system.
Nahyeon Roh, Sejong Oh, Donghun Park
doaj   +1 more source

Investigation of the rotor–obstacle aerodynamic interaction in hovering flight [PDF]

open access: yes, 2018
In this paper, a comprehensive experimental survey of the aerodynamic interaction of a hovering rotor in the proximity of a ground obstacle is described, taking advantage of multiple experimental techniques.
Giuni, Michea   +2 more
core   +2 more sources

Rotorcraft fuselage/main rotor coupling dynamics modelling and analysis [PDF]

open access: yesInternational Journal of Nonlinear Sciences and Numerical Simulation, 2020
AbstractThis article presents the fuselage/main rotor coupling dynamics under a modal analysis to study the modes of oscillation. The authors provide a rotorcraft simulation model that captures complex dynamics, wherein the validation is done with existing theories.
Tomas-Rodriguez, M., Castillo-Rivera, S.
openaire   +2 more sources

Helicopter Safe Landing Trajectory after Main Rotor Actuator Failures

open access: yesApplied Sciences, 2020
Main rotor actuator failure leads to catastrophic accidents for single main rotor helicopters. This paper focuses on safe landing trajectories after an actuator is locked in place by the remaining actuators, without introducing other control inputs.
Yunjie Wang   +3 more
doaj   +1 more source

Thrust pulsation of coaxial main rotor, caused by the blades relative position

open access: yesНаучный вестник МГТУ ГА, 2020
The influence of reciprocal position of the upper rotor blades in respect to the lower rotor blades is characteristic for coaxial main rotor. It is established that the initial azimuth of the blade, for example, of the upper rotor’s which does not ...
B. S. Kritsky   +3 more
doaj   +1 more source

Design of Composite Gyrocopter Main Rotor Blade Involving Rib and Spar Elements [PDF]

open access: yesJournal of Engineering, Project, and Production Management, 2019
Gyrocopter or gyroplane is a type of rotorcraft that uses an unpowered main rotor in free autorotation to develop lift. Gyrocopter rotor blades have smaller cord length and longer span compared to helicopters blades.
Yonas Mitik Degu, Derbew Alebel
doaj   +1 more source

Current Tracking Adaptive Control of Brushless DC Motors

open access: yesInternational Journal of Adaptive Control and Signal Processing, EarlyView.
In this paper, the current tracking for Brushless Direct Current motors is approached considering uncertainty in the parameters of the motor's model. An adaptive control scheme to compensate electrical parameters uncertainty is proposed without requiring any knowledge of the mechanical parameters.
Fernanda Ramos‐García   +3 more
wiley   +1 more source

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