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Application of the Geometrically Exact Intrinsic Beam Model on Rotor Blades

Bleffert, Christian and Dreyer, Lukas and Röhrig-Zöllner, Melven (2023) Application of the Geometrically Exact Intrinsic Beam Model on Rotor Blades. Math 2 Product (M2P), 2023-05-30 - 2023-06-01, Taormina, Italien.

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Abstract

With the Versatile Aeromechanic Simulation Tool (VAST), the German Aerospace Center (DLR) is developing a software framework for the simulation of rotary wing aircraft. One challenge consists of simulating the dynamic behaviour of rotor blades. In general, rotor blades can be considered as flexible beams for which numerous models have been developed in the past. One of them is the geometrically exact intrinsic beam model [2] which is represented by a time dependent hyperbolic system of partial differential equations (PDE) in one space dimension along a reference line of the considered beam. In contrast to other well-known models like the Euler-Bernoulli model or the Timoschenko model, the governing equations of the intrinsic beam model contain non-linearities which makes it a geometrically exact model. Furthermore, it allows for the modelling of initially curved and twisted anisotropic beams making it well-suited for the simulation of rotor blades. In [1], we used a practical formulation of the intrinsic beam model as a system of linear hyperbolic balance laws to derive a discontinuous Galerkin (DG) approach for its discretization. For boundary conditions describing the mechanical setup of a clamped-free beam, we found that this discretization approach is numerically stable if no energy comes from the boundaries of the considered domain. Choosing a DG approach for the discretization of the problem is not only senseful because it is very efficient and helps minimizing the degrees of freedom in the computationally intensive analysis of helicopters. It is also able to represent discontinuities accurately which is interesting for the simulation of rotor blades as for example material parameters might change discontinuously along the blade. For steady-state cases, we show that the intrinsic beam DG method is more accurate than our previous approach using experimental results for a rotating beam in vacuum. In addition, we show first numerical results for simulating the dynamic behaviour and discuss ongoing research and challenges concerning boundary conditions, stability and damping. REFERENCES [1] C. Bleffert. An Energy Stable Discontinuous Galerkin Discretization Approach for the Geometrically Exact Intrinsic Beam Model. Master thesis, University of Cologne, 2022. [2] D. H. Hodges. Geometrically exact, intrinsic theory for dynamics of curved and twisted anisotropic beams. AIAA Journal, 41(6):1131-1137, 2003.

Item URL in elib:https://elib.dlr.de/199089/
Document Type:Conference or Workshop Item (Speech)
Title:Application of the Geometrically Exact Intrinsic Beam Model on Rotor Blades
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Bleffert, ChristianUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Dreyer, LukasUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Röhrig-Zöllner, MelvenUNSPECIFIEDhttps://orcid.org/0000-0001-9851-5886UNSPECIFIED
Date:31 May 2023
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Geometrically Exact Beams, Discontinuous Galerkin, Rotor Blades, Energy Stability
Event Title:Math 2 Product (M2P)
Event Location:Taormina, Italien
Event Type:international Conference
Event Start Date:30 May 2023
Event End Date:1 June 2023
Organizer:ECCOMAS
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space System Technology
DLR - Research area:Raumfahrt
DLR - Program:R SY - Space System Technology
DLR - Research theme (Project):R - Tasks SISTEC
Location: Köln-Porz
Institutes and Institutions:Institute of Software Technology > High-Performance Computing
Institute of Software Technology
Deposited By: Bleffert, Christian
Deposited On:07 Dec 2023 16:29
Last Modified:24 Apr 2024 20:59

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