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Aerodynamic interference between pusher propeller slipstream and an airframe : literature review

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In the article, an aerodynamic interference between pusher propeller slipstream and the airframe of the aircraft powered by it has been presented, based on a literature study. A pusher propeller is one of popular types of the airplane propulsion. It is applied mainly in light sport aircrafts, in the UAVs (Unmanned Aerial Vehicles), unorthodox vehicles, like compound helicopters, canard and joined wing aircrafts etc. The main advantage of pusher propeller is that the engine with the pusher propeller does not affect the visibility from the cockpit and allows placing an electronic equipment in the front part of the UAV’s fuselage. Furthermore, reduced cabin noise and increase in stability due to acting normal force aft of the centre of gravity are other benefits of this configuration. The pusher propeller impact on the airframe, especially on the wing, is qualitatively different from the tractor configuration. Main differences between both propulsions has been discussed, as well as aerodynamic benefits of the pusher propeller – like reduction of separated flow area and extending area of laminar boundary layer. However, an application of pusher propeller may have also negative impact, especially lower performance than tractor propeller. In the article the reasons of this suppression has been briefly discussed.
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  • Institute of Aviation, Department of Aerodynamics Krakowska Av. 110/114, 02-256 Warsaw, Poland tel.: +48 22 8460011 int. 312, fax: +48 22 8463244
Bibliografia
  • [1] Bogdański, K., Rodzewicz, M., Miller, M., Ruchała, P., Koncepcja i realizacja badań zespołu napędowego w tunelu aerodynamicznym, Mechanika w Lotnictwie ML-XVI, pp. 123-134, Warszawa 2014.
  • [2] Bousquet, J.-M., Gardarein, P., Improvements on Computations of High Speed Propeller Unsteady Aerodynamics, Aerospace Science and Technology, Vol. 7, No. 6, pp. 465-472, 2003.
  • [3] Catalano, F.M., On the Effects of an Installed Propeller Slipstream on Wing Aerodynamic Characteristics, Acta Polytechnica, Vol. 44, No. 3, Praha 2004.
  • [4] Chiaramonte, J.-Y., Favier, D., Maresca, C., Agnes, A., Unsteady Interactional Effects Between a Propeller and a Fixed Wing, 9th Applied Aerodynamics Conference, AIAA Paper 91-3231, 1991.
  • [5] Chinwicharnam, K., Thipyopas, C., Comparison of wing–propeller interaction in tractor and pusher configuration, International Journal of Micro Air Vehicles, January-March 2016: pp. 3-20, 2016.
  • [6] Gudmundsson, S., General aviation aircraft design: Applied Methods and Procedures, Butterworth-Heinemann, Oxford 2013.
  • [7] Gunston, B., Cambridge aerospace dictionary, Cambridge University Press, Cambridge 2004.
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  • [9] Lötstedt, P., Accuracy of a propeller model in inviscid flow, Journal of Aircraft, Vol. 32, No. 6, Nov./Dec. 1995.
  • [10] Miranda, L. R., Brennan, J. E., Aerodynamic effects of wing tip mounted propellers and turbines, AIAA 86-1802, pp. 221-228, 1986.
  • [11] Pfeiffer, N., Flowfield study at the propeller disks of a twin pusher canard aircraft, 6th Applied Aerodynamics Conference, Williamsburg 1988.
  • [12] Roosenboom, E., Heider, A., Schröder, A., Investigation of Propeller Slipstream with PIV, Journal of Aircraft, Vol. 46 No. 2, pp. 442-449, 2009.
  • [13] Ruchała, P., An influence of pusher propeller cover on its performance – a concept of wind tunnel investigation, Journal of KONES, Vol. 23, No. 4, pp. 429-434, Warsaw 2016.
  • [14] Ruchała, P., Wind tunnel tests of the pusher propeller – an assessment of accuracy, Journal of KONES, Vol. 23 No. 2, pp. 309-316 Warsaw 2016.
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  • [17] Strzelczyk, P., Wybrane charakterystyki pola prędkości w strumieniu śmigłowym, Prace Instytutu Lotnictwa, 4 (155), pp. 127-135, Warszawa 1998.
  • [18] Veldhuis, L. L. M., Propeller Wing Aerodynamic Interference, Ph.D. Dissertation, Delft University of Technology, Delft, The Netherlands 2005.
  • [19] Veldhuis, L. L. M., Review of propeller-wing aerodynamic interference, Proceedings of 24th ICAS Congress, 2004.
  • [20] Witoszyński, C., Prace wybrane, PWN, Warszawa 1957.
  • [21] Zalewski, W., The impact of propeller on aerodynamics of aircraft (in Polish), Journal of KONBiN, 1(33), 2015.
  • [22] www.wikipedia.org, Quad City Challenger, https://en.wikipedia.org/wiki/Quad_City_Challenger.
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Uwagi
PL
Opracowanie ze środków MNiSW w ramach umowy 812/P-DUN/2016 na działalność upowszechniającą naukę (zadania 2017).
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-47262c08-9597-4dab-896e-b884efdcbf6d
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