Results 21 to 30 of about 189,612 (149)

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

A New Algorithm on Automatic Trimming for Helicopter Rotor Aerodynamic Loads

open access: yesAerospace, 2023
In order to simulate the flight state of the helicopter effectively, it is necessary to trim the helicopter during the forward flight in a wind tunnel test.
Xinfan Yin   +5 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

Hardware-in-the-Loop simulation algorithm for helicopter rotor time-varying echo signals

open access: yesSystems Science & Control Engineering, 2021
The inherent micro-Doppler (m-D) feature of helicopter rotor echoes has been widely used in signal detection and identification. To meet the high accuracy and real-time performance requirements of the hardware-in-the-loop (HIL) simulation, this paper ...
Shihong Chen
doaj   +1 more source

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

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

Research on Calculation Method for Acoustic Scattering of Helicopter Noise

open access: yesXibei Gongye Daxue Xuebao, 2020
A new calculation method of helicopter rotor/fuselage acoustic scattering is developed. Firstly, a CFD analysis model is developed to simulate flow field of the rotor, which is based on the motional embedded grid system and RANS equations, and provides ...

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

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