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Open low speed wind tunnel – design and testing

Treść / Zawartość
Identyfikatory
Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
This paper presents the design method and the construction details of a subsonic low-speed wind tunnel, which has been designed to achieve the flow velocity of 35 m/s in the measurement section with expected uniform velocity field at its inlet. To achieve such objectives a very detailed design was performed using a theoretical 1D analysis and computational fluid dynamics simulations. This approach was applied to improve the flow quality along the wind tunnel sections. When the wind tunnel has been launched a direct comparison of the experimentally measured flow field in the test section and numerical simulation results was conducted. Such comparison of the simulation results with the experimental one is presented in this paper. The obtained results confirm that assumed wind tunnel design method was correct, i.e. the pressure drop in the wind tunnel has been predicted very well and drive system is effective and sufficient to accelerate the airflow to required values.
Słowa kluczowe
Rocznik
Strony
57--70
Opis fizyczny
Bibliogr. 16 poz., rys.
Twórcy
  • Institute of Fluid Flow Machinery, Polish Academy of Sciences, Fiszera 14, 80-231 Gdansk, Poland
  • Institute of Fluid Flow Machinery, Polish Academy of Sciences, Fiszera 14, 80-231 Gdansk, Poland
  • Institute of Fluid Flow Machinery, Polish Academy of Sciences, Fiszera 14, 80-231 Gdansk, Poland
  • Institute of Fluid Flow Machinery, Polish Academy of Sciences, Fiszera 14, 80-231 Gdansk, Poland
  • Institute of Fluid Flow Machinery, Polish Academy of Sciences, Fiszera 14, 80-231 Gdansk, Poland
  • Institute of Fluid Flow Machinery, Polish Academy of Sciences, Fiszera 14, 80-231 Gdansk, Poland
Bibliografia
  • [1] Barlow J.B., Rae Jr W.H., Pope A.: Low-Speed Wind Tunnel Testing. John Wiley and Sons; New York 1999.
  • [2] Bradshaw P., Pankhurst R.C.: The design of low-speed wind tunnels. Prog. Aerosp. Sci. 5(1964), 1–69.
  • [3] Anderson J.D. Jr.: Fundamentals of Aerodynamics (5th Edn.). McGraw-Hill;2011.
  • [4] Kneba Z.: Modeling of the internal combustion engine cooling system. Arch. Thermodyn. 40(2019), 3, 109–121.
  • [5] Muszyński T., Andrzejczyk R., Park W.I., Dorao C.A.: Heat transfer and pressure drop characteristics of the silicone-based plate heat exchanger. Arch. Thermodyn. 40(2019), 1, 127–143.
  • [6] Mehta J., Bradshaw P.: Design rules for small low speed wind tunnels. Aeronaut. J. 83(1979), 827, 443–453.
  • [7] Stathopoulos T.: Design and fabrication of a wind tunnel for building aerodynamics. J. Wind Eng. Ind Aerod. 16(1984), 2–3, 361–376.
  • [8] Cattafesta L., Bahr C., Mathew J.: Fundamentals of wind-tunnel design. In: Encyclopedia of Aerospace Engineering. John Wiley and Sons, Hoboken 2010.
  • [9] Bell J.H., Mehta R.D.: Boundary-layer predictions for small low-speed contractions. AIAA J. 27(1989), 3, 372–374.
  • [10] Noor A., Ed.:Wind Tunnel Designs and their Diverse Engineering Applications. IntechOpen, 2013.
  • [11] Discetti S., Ianiro A., Aref H.: Experimental Aerodynamics. CRC Press – Taylor & Francis Group; Boca Raton 2017.
  • [12] Idelchik I.E.: Handbook of Hydraulic Resistance. Coefficients of Local Resistance and of Friction. US Atomic Energy Commission and the National Science Foundation. Washington DC 1966.
  • [13] Ansys Fluent Fluid Simulation Software https://www.ansys.com/products/fluids/ ansys-fluent (access: 5 Jan. 2020).
  • [14] Ansys Meshing https://www.ansys.com/products/platform/ansys-meshing (access: 5 Jan. 2020).
  • [15] Ochrymiuk T.: Numerical analysis of microholes film/effusion cooling effectiveness. J. Therm. Sci. 26(2017), 5, 459–464.
  • [16] Szwaba R., Ochrymiuk T., Lewandowski T., Czerwinska J.: Experimental investigation of microscale effects in perforated plate aerodynamics. J. Fluids Eng. 135(2013), 12, 121104-1-10
Uwagi
Opracowanie rekordu ze środków MNiSW, umowa Nr 461252 w ramach programu "Społeczna odpowiedzialność nauki" - moduł: Popularyzacja nauki i promocja sportu (2021).
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-495037b5-6c24-4db2-a074-dd65e77625a8
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