Results 21 to 30 of about 30,315 (234)

An Analytical Method for Coaxial Helicopter Ground Resonance [PDF]

open access: yesMATEC Web of Conferences, 2020
A time-frequency analytical method is presented to analyze physical mechanism of coaxial helicopter ground resonance. Eigenvalue calculation and numerical integration of disturbance equations of motions are used to obtain modal characters and time-domain
Liu Xiangyi   +4 more
doaj   +1 more source

Flight Mechanics Modeling of the New Configuration Tilt-rotor

open access: yesHangkong gongcheng jinzhan, 2019
The flight mechanical model of tilt-rotor UAV is the basis of designing flight control rate and analyzing flight characteristics.Based on the engineering reality, the nonlinear flight mechanics model of a new configuration tilt-rotor UAV is set up ...
Zhang Lian   +3 more
doaj   +1 more source

Fracture fault analysis of tail rotor on a helicopter

open access: yesHangkong gongcheng jinzhan, 2023
Finding out the reason of the fracture fault of tail rotor on a helicopter is of practical significance for using and maintaining the helicopter and is of significant reference for improving safety of new type helicopter. The fracture fault of tail rotor
HOU Bo   +3 more
doaj   +1 more source

Quad-Rotor Helicopter Autonomous Navigation Based on Vanishing Point Algorithm

open access: yesJournal of Applied Mathematics, 2014
Quad-rotor helicopter is becoming popular increasingly as they can well implement many flight missions in more challenging environments, with lower risk of damaging itself and its surroundings.
Jialiang Wang   +5 more
doaj   +1 more source

Optimal design of fixed-pitch coaxial-rotor helicopter by using Particle Swarm Optimization

open access: yesNihon Kikai Gakkai ronbunshu, 2016
In this study, the optimal mechanical design method for fixed-pitch coaxial-rotor helicopter is proposed. The fixed-pitch coaxial-rotor helicopter has several advantages compared with other type helicopters.
Masahiro TATSUNO   +3 more
doaj   +1 more source

Numerical investigation for coupled rotor/ship flowfield using two models based on the momentum source method

open access: yesEngineering Applications of Computational Fluid Mechanics, 2021
The coupled rotor/ship flowfield is investigated using the Navier–Stokes solver when the helicopter rotor hovers in the ship’s airwake. The solid rotor model (SRM) and virtual rotor model (VRM) are employed, considering the different types of rotor ...
Zhao Dingxuan   +3 more
doaj   +1 more source

Modelling and simulation of a quad-rotor helicopter [PDF]

open access: yes, 2012
Small size quad-rotor helicopters are often used due to the simplicity of their construction and maintenance, their ability to hover and also to take-off and land vertically.
Bousbaine, Amar   +2 more
core   +2 more sources

RESULTS OF THE FIRST MI-171A2 FLYING LABORATORY TEST PHASE

open access: yesНаучный вестник МГТУ ГА, 2014
The present publication describes the results of the first stage of the flying laboratory (Mi-171 helicopter) flight tests performed at Mil Moscow Helicopter Plant, JSC facilities. Main rotor components with blades made of polymer composite materials and
V. A. Ivchin, K. Y. Samsonov
doaj   +1 more source

Numerical modelling of the aerodynamic interference between helicopter and ground obstacles [PDF]

open access: yes, 2017
Helicopters are frequently operating in confined areas where the complex flow fields that develop in windy conditions may result in dangerous situations.
Barakos, George N.   +3 more
core   +1 more source

The influence of helicopter tail rotor parameters on RCS

open access: yesHangkong gongcheng jinzhan
High requirements have been placed on the stealth performance of armed helicopters during wartime missions,in order to reduce the probability of the helicopter being found during the task,based on geometric optics method and consistent diffraction theory,
ZHAO Qijun
doaj   +1 more source

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