• Nie Znaleziono Wyników

Fluid-Structure Interaction of Inflatable Wing Sections

N/A
N/A
Protected

Academic year: 2021

Share "Fluid-Structure Interaction of Inflatable Wing Sections"

Copied!
1
0
0

Pełen tekst

(1)

Mikko Folkersma PhD Researcher Delft University of Technology Faculty of Aerospace Engineering

Wind Energy Research Group

Kluyverweg 1 2629 HS Delft The Netherlands

m.a.m.folkersma@tudelft.nl kitepower.tudelft.nl

Fluid-Structure Interaction of Inflatable Wing Sections

Mikko Folkersma1, Paul Thedens1,2, Roland Schmehl1, Axelle Vire1

1Delft University of Technology 2Skysails Power GmbH

We investigate inflatable kites made of membranes such as ram-air [1] and leading edge inflatable [2] kites. The kites are very flexible and therefore exhibit a strong cou-pling between fluid and structure. An accurate aerody-namic model is essential to design kites which are aero-dynamically efficient and of high steering capability. In this work, a fluid-structure interaction methodology is developed to study the steady-state aerodynamics of in-flatable kites. The aerodynamic load distribution is calcu-lated using computational fluid dynamics toolbox Open-FOAM. Steady-state solver with RANS based turbulence model k − ω SST is used. The structural deformation is calculated with mem4py [2] finite element solver for membranes which uses dynamic relaxation method to find the static shape. The two solvers are coupled with preCICE [3] coupling tool. Each solver is connected to preCICE through an adapter and thereafter preCICE takes care of the coupling such as the parallel communication, the data mapping for non-matching meshes and the cou-pling algorithm to accelerate the convergence.

The fluid and the structure solvers are validated against relevant experiments and the coupled simulation frame-work is used to study the aerodynamics of a ram-air wing section with uniform pressure inside. The results show large deformations and therefore the aerodynamic loads highly depend on the structural deformations. The cou-pled framework shows a good compromise between fi-delity and efficiency.

Pressure coefficient around the kite section and streamlines at the symmetry plane with α = 10.

References:

[1] Thedens, P. and de Oliveira, G. and Schmehl, R.: Ram-air kite air-foil and reinforcements optimization for airborne wind energy ap-plications. Wind Energy 22(5), 653-665 (2019)

[2] Oehler, J. and Schmehl, R.: Aerodynamic characterization of a soft kite by in situ flow measurement. Wind Energy Science 4, 1-21 (2019)

[3] Bungartz, H. and Lindner, F. and Gatzhammer, B. and Mehl, M. and Scheufele, K. and Shukaev, A. and Uekermann, B.: preCICE ś A fully parallel library for multi-physics surface coupling. Computers and Fluids 141, 250-258 (2016)

Cytaty

Powiązane dokumenty

Umieralność ludności jest najbardziej newralgicznym problemem społe­ cznym, który nadal jest niedostatecznie rozpoznany w zakresie mechani­ zmów i przyczyn go warunkujących.

Nie jest jednak jasne, czy Miller uważa, że jest do tego zmuszony jako autor przez potrzebę znalezienia pewnego wzoru, czy jest zmuszony przez impuls Foucaulta

The rest of the volume consists of essays devoted to writing in English (contributions by Dagmara Drewniak, Agnieszka Rzepa, Ewa Bodal and Anna Branach-Kallas), French

The programs (incl. conference, international travel, library research, and lecture tours grants), however, were suspended due to Canadian government’s decision to cease

To introduce Riemann solutions on the discontinuous boundaries, the 1D membrane equation is written as a system of first order wave equations.. Subsequently, the string deflection

Skoro więc Chrystus jest źródłem łaski, a obdarzenie nią prowadzi człowieka do złączenia z Nim oraz do wcielenia w Jego ciało, to zagadnienie możliwości zbawienia tych,

The competition among parcel delivery services is severe giving them hard challenges to operate cost-efficient and meanwhile perform more sustainable, especially for the last

The structural model- ing is done using the commercial solver ABAQUS (Solver- FEA) with a finite element analysis (FEA).. The