Results 11 to 20 of about 15,230 (231)

Helicopter performance enhancement by alleviating retreating blade stall using active flow control

open access: yesScientific African, 2023
In this study, a model was created numerically to study the effect of active flow control on helicopter blade to improve the retreating blade stall. Active flow control is applied to helicopter blades to improve retreating blade stall along with the ...
Tarek Mokhtar Tawfik Soltan   +1 more
doaj   +1 more source

Feature Extraction Method of Helicopter Target Based on Flicker Phenomenon Combined With Phase Compensation

open access: yesIEEE Access, 2022
For the typical multi-component periodic micro-Doppler signal parameter estimation, a helicopter rotor feature extraction method based on flicker phenomenon and phase compensation is proposed in this paper.
Saiqiang Xia   +6 more
doaj   +1 more source

Finite Element Framework for Efficient Design of Three Dimensional Multicomponent Composite Helicopter Rotor Blade System

open access: yesEng, 2021
In the present study, a three-dimensional finite element framework has been developed to model a full-scale multilaminate composite helicopter rotor blade. Tip deformation and stress behavior have been analyzed for external aerodynamic loading conditions
Arunabha M. Roy
doaj   +1 more source

Fracture analysis of AA6061-graphite composite for the application of helicopter rotor blade

open access: yesFracture and Structural Integrity, 2021
The main objective of the work is to study the fracture behavior of AA6061-graphite material using both experimental technique and finite element simulation by considering helicopter rotor blade as a case study.
Saleemsab Doddamani   +3 more
doaj   +1 more source

Reducing Helicopter Vibration Loads by Individual Blade Control with Genetic Algorithm

open access: yesMachines, 2022
A rotor that can realize individual blade pitch control was designed. This paper focuses on finding the trend of helicopter vibration loads after applying multiple high-order harmonic control.
Renguo Yang   +3 more
doaj   +1 more source

Chord Morphing for Helicopter Rotor Blades [PDF]

open access: yesASME 2019 Conference on Smart Materials, Adaptive Structures and Intelligent Systems, 2019
Abstract Since helicopter rotors have different demands from different flight stats, the final design is always a compromise between flight stats such as hover and fast forward flight. Two of the design parameters are twist and chord length.
Riemenschneider, Johannes   +3 more
openaire   +2 more sources

CALCULATED RESEARCH OF INFLUENCE OF HELICOPTER MAIN ROTORS GEOMETRY ON THE EFFICIENCY IN HOVER MODE BASED ON THE NONLINEAR VORTEX MODEL

open access: yesНаучный вестник МГТУ ГА, 2018
The efficiency of the helicopter main rotor in the hover mode is very important, because this mode essentially determines the performance characteristics of the helicopter.
Y. M. Ignatkin   +2 more
doaj   +1 more source

Numerical Simulation of Helicopter Rotor Performance Degradation in Natural Rain Encounter

open access: yesInternational Journal of Aerospace Engineering, 2021
Sustained flight operation in the rain conditions is still a challenge to a pilot. This problem can be mainly attributed to the aerodynamic performance degradation of aircraft.
Guozhi Li, Yihua Cao
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

Dynamics of helicopter rotor blades

open access: yesComputers & Structures, 1988
A rotating blade finite element with coupled bending, torsion and axial stretching degrees-of-freedom is developed. APL is used for symbolic manipulations required for the development of the element. The element is implemented in MSC/NASTRAN to generate the numerical results.
Magari, P. J.   +2 more
openaire   +1 more source

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