Szczegóły

Tytuł artykułu

Identification of unsteady effects in the flow through a centrifugal fan using CFD/CAA methods

Tytuł czasopisma

Archives of Thermodynamics

Rocznik

2021

Wolumin

vol. 42

Numer

No 4

Afiliacje

Pritz, Balazs : Institute of Thermal Turbomachinery, Karlsruhe Institute of Technology, Kaiserstraße 12 D-76131 Karlsruhe, Germany ; Probst, Matthias : Institute of Thermal Turbomachinery, Karlsruhe Institute of Technology, Kaiserstraße 12 D-76131 Karlsruhe, Germany ; Wiśniewski, Piotr : Department of Power Engineering and Turbomachinery, Silesian University of Technology, Poland ; Dykas, Sławomir : Department of Power Engineering and Turbomachinery, Silesian University of Technology, Poland ; Majkut, Mirosław : Department of Power Engineering and Turbomachinery, Silesian University of Technology, Poland ; Smołka, Krystian : Department of Power Engineering and Turbomachinery, Silesian University of Technology, Poland

Autorzy

Słowa kluczowe

Centrifugal fan ; CFD ; CAA

Wydział PAN

Nauki Techniczne

Zakres

169-181

Wydawca

The Committee of Thermodynamics and Combustion of the Polish Academy of Sciences and The Institute of Fluid-Flow Machinery Polish Academy of Sciences

Bibliografia

[1] Dykas S., Wróblewski W., Rulik S., Chmielniak T.: Numerical method for modelling of acoustic waves propagation. Arch. Acoust. 35(2010), 1, 35–48.
[2] Fortuna S., Sobczak K.: Numerical and experimental investigations of the flow in radial fan. Mechanics 27(2008), 4, 138–143
[3] Moon Y.J., Cho Y., Nam H.S.: Computation of unsteady viscous flow and aeroacoustic noise of the cross flow fan. Comput. Fluids 32(2003), 7, 995–1015.
[4] Rulik S., Dykas S., Wroblewski W.: Modelling of aerodynamic noise using hybrid SAS and DES methods. In: Proc. ASME Turbo Expo 2010: Power for Land, Sea and Air, Glasgow, June 14–18, 2010, 7(2010), 2835–2844., GT2010-2269.
[5] Stasko T., Dykas S., Majkut M., Smolka K.: An attempt to evaluate the cycloidal rotor fan performance. Open J. Fluid Dynam. 9(2019), 4.
[6] Benedek T., Vad J.: Beamforming based extension of semi-empirical noise modelling for low-speed axial flow fans. Appl. Acoust. 178(2021), 108018.
[7] Jiang H., Wang Q., Zheng T.F., Tu C.X., Zhang K.: PIV measurement of internal flow field in a range hood. In: Energy and Mechanical Engineering (S.Y. Liang, Ed.), 2015 Int. Conf. on Energy and Mechanical Engineering, Wuhan, 17-18 Oct. 2015, World Scientific, 2016, 570–575.
[8] Probst M., Pritz B.: Quantitative validation of CFD-simulation against PIV data for a centrifugal fan. In: Proc. 14th Int. Symp. on Experimental Computational Aerothermodynamics of Internal Flows, Gdansk 8-11 July 2019.
[9] Neise W., Michel U.: Aerodynamic Noise of Turbomachines. DLR-Interner Bericht, Berlin 1994.
[10] Jeon W.H., Lee D.J., Rhee H.: An application of the acoustic similarity law to the numerical analysis of centrifugal fan noise. JSME Int. J. C-mech Sy. 47(2004), 3, 845–851.
[11] Kissner C., Guerin S.: Comparison of predicted fan broadband noise using a twoversus a three-dimensional synthetic turbulence method. J. Sound Vib. 508(2021), 116221.
[12] Jaron R., Herthum H., Franke M., Moreau A., Guerin S.: Impact of turbulence models on RANS-informed prediction of fan broadband interaction noise. In: Proc. 12th Eur. Turbomachinery Conference (ETC), Stockholm, 3-7 April, 2017.
[13] Carolus T.: Theoretische und experimentelle Untersuchung des Pumpens von lufttechnischen Anlagen mit Radialventilatoren. PhD thesis, Karlsruhe University of Applied Sciences, Karlsruhe 1984.
[14] Blazquez-Navarro R., Corral R.: Prediction of fan acoustic blockage on fan/outlet guide vane broadband interaction noise using frequency domain linearized Navier–Stokes solvers. J. Sound Vib. 508(2021), 116033.
[15] Ffowcs-Williams J.E., Hawkings D.L.: Sound generation by turbulence and surfaces in arbitrary motion. Philos. T.R. Soc. Lond. S-A, 264(1969), 1151, 321–342.
[16] Lighthill M.J.: On sound generated aerodynamically. I. General theory. Proc. R. Soc. Lon. Ser.-A 211(1952) 1107, 564–587
[17] Menter F.R., Egorov Y.: A scale-adaptive simulation model using two-equation models. In: Proc. 43th AIAA Aerospace Sciences Meeting and Exhibit, Reno, 10-13 Jan. 2005, AIAA 2005-1095.
[18] Ansys Fluent Theory Guide, 2021R1. https://www.ansys.com (acessed 1 July 12021).

Data

2022.01.17

Typ

Article

Identyfikator

DOI: 10.24425/ather.2021.139657 ; ISSN 1231-0956 ; eISSN 2083-6023

Rada naukowa

International Advisory Board

J. Bataille, Ecole Central de Lyon, Ecully, France

A. Bejan, Duke University, Durham, USA

W. Blasiak, Royal Institute of Technology, Stockholm, Sweden

G. P. Celata, ENEA, Rome, Italy

L.M. Cheng, Zhejiang University, Hangzhou, China

M. Colaco, Federal University of Rio de Janeiro, Brazil

J. M. Delhaye, CEA, Grenoble, France

M. Giot, Université Catholique de Louvain, Belgium

K. Hooman, University of Queensland, Australia

D. Jackson, University of Manchester, UK

D.F. Li, Kunming University of Science and Technology, Kunming, China

K. Kuwagi, Okayama University of Science, Japan

J. P. Meyer, University of Pretoria, South Africa

S. Michaelides, Texas Christian University, Fort Worth Texas, USA

M. Moran, Ohio State University, Columbus, USA

W. Muschik, Technische Universität Berlin, Germany

I. Müller, Technische Universität Berlin, Germany

H. Nakayama, Japanese Atomic Energy Agency, Japan

A. Nenarokomov, Moscow Aviation Institute, Russia

S. Nizetic, University of Split, Croatia

H. Orlande, Federal University of Rio de Janeiro, Brazil

M. Podowski, Rensselaer Polytechnic Institute, Troy, USA

A. Rusanov, Institute for Mechanical Engineering Problems NAS, Kharkiv, Ukraine

M. R. von Spakovsky, Virginia Polytechnic Institute and State University, Blacksburg, USA

A. Vallati, Sapienza University of Rome, Italy

H.R. Yang, Tsinghua University, Beijing, China



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