Helicopter Rotor Sailing by Non-Smooth Dynamics Co-Simulation

This paper presents the application of a co-simulation approach for the simulation of frictional contact in general-purpose multibody dynamics to a rotorcraft dynamics problem. The proposed approach is based on the co-simulation of a main problem, which is described and solved as a set of differenti...

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Main Authors: Fancello Matteo, Morandini Marco, Masarati Pierangelo
Format: Article
Language:English
Published: Polish Academy of Sciences 2014-08-01
Series:Archive of Mechanical Engineering
Subjects:
Online Access:http://www.degruyter.com/view/j/meceng.2014.61.issue-2/meceng-2014-0015/meceng-2014-0015.xml?format=INT
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spelling doaj-cd94ce265f924abfae959013a5526db62020-11-25T03:02:23ZengPolish Academy of SciencesArchive of Mechanical Engineering 2300-18952014-08-0161225326810.2478/meceng-2014-0015meceng-2014-0015Helicopter Rotor Sailing by Non-Smooth Dynamics Co-SimulationFancello Matteo0Morandini Marco1Masarati Pierangelo2Politecnico di Milano, Dipartimento di Scienze e Tecnologie Aerospaziali, via La Masa 34, 20156 Milano - ItalyPolitecnico di Milano, Dipartimento di Scienze e Tecnologie Aerospaziali, via La Masa 34, 20156 Milano - ItalyPolitecnico di Milano, Dipartimento di Scienze e Tecnologie Aerospaziali, via La Masa 34, 20156 Milano - ItalyThis paper presents the application of a co-simulation approach for the simulation of frictional contact in general-purpose multibody dynamics to a rotorcraft dynamics problem. The proposed approach is based on the co-simulation of a main problem, which is described and solved as a set of differential algebraic equations, with a subproblem that is characterized by nonsmooth dynamics events and solved using a timestepping technique. The implementation and validation of the formulation is presented. The method is applied to the analysis of the droop and anti-flap contacts of helicopter rotor blades. Simulations focusing on the problem of blade sailing are conducted to understand the behavior and assess the validity of the method. For this purpose, the results obtained using a contact model based on Hertzian reaction forces at the interface are compared with those of the proposed approach.http://www.degruyter.com/view/j/meceng.2014.61.issue-2/meceng-2014-0015/meceng-2014-0015.xml?format=INTmultibody dynamicsnonsmooth dynamicscontacttimestepping methodsco-simulation
collection DOAJ
language English
format Article
sources DOAJ
author Fancello Matteo
Morandini Marco
Masarati Pierangelo
spellingShingle Fancello Matteo
Morandini Marco
Masarati Pierangelo
Helicopter Rotor Sailing by Non-Smooth Dynamics Co-Simulation
Archive of Mechanical Engineering
multibody dynamics
nonsmooth dynamics
contact
timestepping methods
co-simulation
author_facet Fancello Matteo
Morandini Marco
Masarati Pierangelo
author_sort Fancello Matteo
title Helicopter Rotor Sailing by Non-Smooth Dynamics Co-Simulation
title_short Helicopter Rotor Sailing by Non-Smooth Dynamics Co-Simulation
title_full Helicopter Rotor Sailing by Non-Smooth Dynamics Co-Simulation
title_fullStr Helicopter Rotor Sailing by Non-Smooth Dynamics Co-Simulation
title_full_unstemmed Helicopter Rotor Sailing by Non-Smooth Dynamics Co-Simulation
title_sort helicopter rotor sailing by non-smooth dynamics co-simulation
publisher Polish Academy of Sciences
series Archive of Mechanical Engineering
issn 2300-1895
publishDate 2014-08-01
description This paper presents the application of a co-simulation approach for the simulation of frictional contact in general-purpose multibody dynamics to a rotorcraft dynamics problem. The proposed approach is based on the co-simulation of a main problem, which is described and solved as a set of differential algebraic equations, with a subproblem that is characterized by nonsmooth dynamics events and solved using a timestepping technique. The implementation and validation of the formulation is presented. The method is applied to the analysis of the droop and anti-flap contacts of helicopter rotor blades. Simulations focusing on the problem of blade sailing are conducted to understand the behavior and assess the validity of the method. For this purpose, the results obtained using a contact model based on Hertzian reaction forces at the interface are compared with those of the proposed approach.
topic multibody dynamics
nonsmooth dynamics
contact
timestepping methods
co-simulation
url http://www.degruyter.com/view/j/meceng.2014.61.issue-2/meceng-2014-0015/meceng-2014-0015.xml?format=INT
work_keys_str_mv AT fancellomatteo helicopterrotorsailingbynonsmoothdynamicscosimulation
AT morandinimarco helicopterrotorsailingbynonsmoothdynamicscosimulation
AT masaratipierangelo helicopterrotorsailingbynonsmoothdynamicscosimulation
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