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Experimental Determination of the Effect of Floats on Aerodynamic Characteristics of the “OSA” Aircraft in Asymmetric Flow

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EN
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This study provides the results of experimental tests of the effect of floats on the aerodynamic characteristics of the “OSA” plane in an asymmetric flow. The tests were carried out in a low-speed wind tunnel owned by Institute of Aviation Technology, Faculty of Mechatronics, Armament and Aerospace (FMAA), Military University of Technology (MUT, Warsaw, Poland). The model of “OSA” was tested at dynamic pressure q = 500 Pa within the range of slip angles β = -28°÷28°. The tests were carried out for the plane model in the so-called “plain” configuration, i.e. at non-deflected control surfaces and wing mechanisation elements. The model was tested in two variants – with floats and without floats. The effect of deflection of the flaps, ailerons and rudder on the aerodynamic characteristics of the test model was also examined. The obtained values of drag coefficient, lateral force coefficient and yawing moment coefficient are presented in the form of tables and graphs. The tests showed that the floats had a significant impact on the curves of the characteristics. They result in a considerable increase of the value of the drag coefficient and in a deterioration of weathercock stability.
Rocznik
Strony
27--44
Opis fizyczny
Bibliogr. 13 poz., fot., rys., tab., wykr.
Twórcy
  • Military University of Technology, Faculty of Mechatronics, Armament and Aerospace, 2 Sylwestra Kaliskiego Str., 00-908 Warsaw, Poland
  • Military University of Technology, Faculty of Mechatronics, Armament and Aerospace, 2 Sylwestra Kaliskiego Str., 00-908 Warsaw, Poland
  • Military University of Technology, Faculty of Mechatronics, Armament and Aerospace, 2 Sylwestra Kaliskiego Str., 00-908 Warsaw, Poland
Bibliografia
  • [1] Krzyżanowski, Adam. 2009. Mechanika lotu. Warszawa: Wydawnictwo Wojskowej Akademii Technicznej.
  • [2] Pope, Alan. 1954. Wind-Tunnel Testing. New York: John Wiley & Sons.
  • [3] Olejnik, Aleksander, Łukasz Kiszkowiak, Adam Dziubiński. 2016. Problemy analizy aerodynamicznej samolotów klasy general aviation. W Mechanika w lotnictwie ML-XVII 2016 (Tom II) : 85-102. Warszawa: Polskie Towarzystwo Mechaniki Teoretycznej i Stosowanej.
  • [4] Olejnik, Aleksander, Łukasz Kiszkowiak, Adam Dziubiński. 2017. "Problemy analizy aerodynamicznej samolotów klasy General Aviation z wykorzystaniem metod numerycznej mechaniki płynów”. Mechanik 8-9 : 802-804
  • [5] Chicken, S. H. 1999. Conceptual design methodologies for waterborne and amphibious aircraft. Canfield University.
  • [6] Darrol, Stinton. 1987."Aero-marine design and flying qualities of floatplanes and flying-boats", Aeronautical Journal.
  • [7] Hu, Qi, Bin Wu, Ming-Zhen Wang, Miao Huang, Rong Jiang. 2019. „Numerical Simulation of Wave Landing Loads Characteristics of Twin-Float Seaplane”. IOP Conf. Ser.: Mater. Sci. Eng. 692 : 012024-1-7.
  • [8] Kaczmarczyk, Jan, Jan Maruszkiewicz. 1970. Poradnik do ćwiczeń laboratoryjnych z mechaniki płynów. Warszawa: Wydawnictwo Wojskowej Akademii Technicznej.
  • [9] Frant, Michał, Stanisław Wrzesień, Maciej Majcher. 2021. „Experimental Determination of the Impact of Floats on the Aerodynamic Characteristics of an OSA Model in Symmetric Flow”. Problemy mechatroniki. Uzbrojenie, lotnictwo, inżynieria bezpieczeństwa / Problems of Mechatronics. Armament, Aviation, Safety Engineering 12 (1) : 41-58.
  • [10] Penkchjerst, Richard, D. Cholder. 1955. Wind tunnel experiment implementation technique (in Russian). Moscow: Izdatielstwo Innostrannoj Literatury.
  • [11] Ardiansyah, Riki, Mohammad Adhitya. 2019. „Simulation of float of 19 passenger aircraft during landing on water surface”. IOP Conf. Ser.: Mater. Sci. Eng. 694 : 012005-1-9.
  • [12] Seaplane, Skiplane, and Float/Ski Equipped Helicopters Operations Handbook. 2004, Washington, U. S. Department of Transportation, Federal Aviation Administration
  • [13] Gudmundsson, Snorii. 2014. General Aviation Aircraft Design. Applied Methods and Procedures. Oxford: Elsevier.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-3a359910-fee9-46ea-8c56-01326c10d6fa
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